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Commit b2540417 authored by Zhang Xin's avatar Zhang Xin
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# g_cssc
# lambda_Angst throughput
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Instrument/throughputs/i_throughput.txt 0 → 100644
View file @ b2540417
# i_cssc
# lambda_Angst throughput
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Instrument/throughputs/nuv_throughput.txt 0 → 100644
View file @ b2540417
# NUV_cssc
# lambda_Angst throughput
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Instrument/throughputs/r_throughput.txt 0 → 100644
View file @ b2540417
# r_cssc
# lambda_Angst throughput
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Instrument/throughputs/sky_emiss_hubble_50_50_A.dat 0 → 100644
View file @ b2540417
# huble skybackground mean level, earthshine + zodical light
#wavelength(A) flux(photon/s/A/arcsec^2/m^2)
1000.0 6.062014541418706e-09
1005.0 1.1324002246856417e-08
1010.0 1.6638046446152143e-08
1015.0 2.2004147139305884e-08
1020.0 2.7422304326317643e-08
1025.0 3.289251800718741e-08
1030.0 3.8414788181915204e-08
1035.0 4.398911485050101e-08
1040.0 4.961549801294483e-08
1045.0 5.5293937669246676e-08
1050.0 6.102443381940653e-08
1055.0 6.68069864634244e-08
1060.0 7.26415956013003e-08
1065.0 7.852826123303418e-08
1070.0 8.446698335862612e-08
1075.0 9.045776197807603e-08
1080.0 9.650059709138398e-08
1085.0 1.0259548869854993e-07
1090.0 1.0874243679957394e-07
1095.0 1.1494144139445595e-07
1100.0 1.2119250248319594e-07
1105.0 1.1621516866148182e-07
1110.0 1.1118780580055496e-07
1115.0 1.0611041390041543e-07
1120.0 1.009829929610632e-07
1125.0 9.580554298249834e-08
1130.0 9.057806396472076e-08
1135.0 8.530055590773051e-08
1140.0 7.997301881152757e-08
1145.0 7.459545267611195e-08
1150.0 6.916785750148364e-08
1155.0 6.369023328764268e-08
1160.0 5.8162580034589e-08
1165.0 5.2584897742322656e-08
1170.0 4.695718641084362e-08
1175.0 4.127944604015191e-08
1180.0 3.5551676630247506e-08
1185.0 2.977387818113043e-08
1190.0 2.394605069280067e-08
1195.0 1.8068194165258228e-08
1200.0 1.2140308598503108e-08
1205.0 1.1911173524700924e-08
1210.0 1.1679717125645938e-08
1215.0 1.144593940133815e-08
1220.0 1.1209840351777559e-08
1225.0 1.0971419976964167e-08
1230.0 1.0730678276897972e-08
1235.0 1.0487615251578977e-08
1240.0 1.0242230901007181e-08
1245.0 9.994525225182583e-09
1250.0 9.744498224105179e-09
1255.0 9.49214989777498e-09
1260.0 9.237480246191975e-09
1265.0 8.980489269356168e-09
1270.0 8.721176967267561e-09
1275.0 8.45954333992615e-09
1280.0 8.19558838733194e-09
1285.0 7.929312109484926e-09
1290.0 7.660714506385111e-09
1295.0 7.389795578032495e-09
1300.0 7.116555324427076e-09
1305.0 6.840993745568856e-09
1310.0 6.5631108414578336e-09
1315.0 6.282906612094011e-09
1320.0 6.000381057477383e-09
1325.0 5.715534177607957e-09
1330.0 5.428365972485726e-09
1335.0 5.138876442110697e-09
1340.0 4.847065586482863e-09
1345.0 4.552933405602229e-09
1350.0 4.256479899468791e-09
1355.0 3.9577050680825545e-09
1360.0 3.656608911443514e-09
1365.0 3.3531914295516723e-09
1370.0 3.0474526224070294e-09
1375.0 2.7393924900095834e-09
1380.0 2.4290110323593374e-09
1385.0 2.1163082494562875e-09
1390.0 1.801284141300438e-09
1395.0 1.483938707891785e-09
1400.0 1.1642719492303297e-09
1405.0 1.302827183295651e-09
1410.0 1.442338980492367e-09
1415.0 1.5828073408204775e-09
1420.0 1.7242322642799823e-09
1425.0 1.866613750870882e-09
1430.0 2.009951800593176e-09
1435.0 2.154246413446864e-09
1440.0 2.2994975894319473e-09
1445.0 2.445705328548425e-09
1450.0 2.5928696307962963e-09
1455.0 2.7409904961755633e-09
1460.0 2.890067924686224e-09
1465.0 3.040101916328279e-09
1470.0 3.1910924711017297e-09
1475.0 3.343039589006575e-09
1480.0 3.495943270042813e-09
1485.0 3.649803514210447e-09
1490.0 3.804620321509474e-09
1495.0 3.960393691939896e-09
1500.0 4.117123625501715e-09
1505.0 8.93940767390179e-09
1510.0 1.3793642289099087e-08
1515.0 1.8679827471093606e-08
1520.0 2.3597963219885345e-08
1525.0 2.8548049535474305e-08
1530.0 3.353008641786049e-08
1535.0 3.8544073867043887e-08
1540.0 4.359001188302451e-08
1545.0 4.866790046580235e-08
1550.0 5.3777739615377417e-08
1555.0 5.8919529331749705e-08
1560.0 6.409326961491921e-08
1565.0 6.929896046488596e-08
1570.0 7.453660188164988e-08
1575.0 7.980619386521105e-08
1580.0 8.510773641556946e-08
1585.0 9.044122953272506e-08
1590.0 9.58066732166779e-08
1595.0 1.0120406746742795e-07
1600.0 1.0663341228497521e-07
1605.0 2.656467766234215e-07
1610.0 4.2564880223865926e-07
1615.0 5.866394891306888e-07
1620.0 7.486188372995099e-07
1625.0 9.115868467451226e-07
1630.0 1.075543517467527e-06
1635.0 1.2404888494667231e-06
1640.0 1.4064228427427105e-06
1645.0 1.5733454972954894e-06
1650.0 1.7412568131250607e-06
1655.0 1.9101567902314226e-06
1660.0 2.080045428614577e-06
1665.0 2.250922728274523e-06
1670.0 2.4227886892112605e-06
1675.0 2.595643311424789e-06
1680.0 2.76948659491511e-06
1685.0 2.9443185396822223e-06
1690.0 3.120139145726126e-06
1695.0 3.2969484130468213e-06
1700.0 3.474746341644308e-06
1705.0 3.6828985428956737e-06
1710.0 3.892211637748622e-06
1715.0 4.102685626203155e-06
1720.0 4.3143205082592715e-06
1725.0 4.527116283916972e-06
1730.0 4.741072953176257e-06
1735.0 4.956190516037125e-06
1740.0 5.172468972499578e-06
1745.0 5.389908322563615e-06
1750.0 5.608508566229232e-06
1755.0 5.828269703496438e-06
1760.0 6.0491917343652265e-06
1765.0 6.271274658835598e-06
1770.0 6.494518476907555e-06
1775.0 6.7189231885810926e-06
1780.0 6.944488793856216e-06
1785.0 7.171215292732926e-06
1790.0 7.399102685211216e-06
1795.0 7.6281509712910916e-06
1800.0 7.85836015097255e-06
1805.0 8.07091933107771e-06
1810.0 8.284535189309783e-06
1815.0 8.49920772566877e-06
1820.0 8.714936940154672e-06
1825.0 8.931722832767487e-06
1830.0 9.149565403507218e-06
1835.0 9.368464652373863e-06
1840.0 9.588420579367423e-06
1845.0 9.809433184487896e-06
1850.0 1.0031502467735282e-05
1855.0 1.0254628429109583e-05
1860.0 1.0478811068610799e-05
1865.0 1.0704050386238928e-05
1870.0 1.0930346381993973e-05
1875.0 1.115769905587593e-05
1880.0 1.1386108407884804e-05
1885.0 1.1615574438020591e-05
1890.0 1.184609714628329e-05
1895.0 1.2077676532672904e-05
1900.0 1.2310312597189432e-05
1905.0 1.2712087023747278e-05
1910.0 1.3115800446982773e-05
1915.0 1.3521452866895907e-05
1920.0 1.3929044283486693e-05
1925.0 1.433857469675512e-05
1930.0 1.4750044106701198e-05
1935.0 1.5163452513324916e-05
1940.0 1.5578799916626283e-05
1945.0 1.59960863166053e-05
1950.0 1.6415311713261957e-05
1955.0 1.6836476106596262e-05
1960.0 1.7259579496608216e-05
1965.0 1.7684621883297813e-05
1970.0 1.8111603266665053e-05
1975.0 1.8540523646709943e-05
1980.0 1.8971383023432478e-05
1985.0 1.940418139683266e-05
1990.0 1.9838918766910488e-05
1995.0 2.027559513366596e-05
2000.0 2.071421049709908e-05
2005.0 2.327957785004678e-05
2010.0 2.5857481770708722e-05
2015.0 2.8447922259084894e-05
2020.0 3.105089931517531e-05
2025.0 3.3666412938979966e-05
2030.0 3.6294463130498865e-05
2035.0 3.893504988973199e-05
2040.0 4.158817321667937e-05
2045.0 4.425383311134099e-05
2050.0 4.6932029573716845e-05
2055.0 4.9622762603806926e-05
2060.0 5.232603220161126e-05
2065.0 5.504183836712983e-05
2070.0 5.7770181100362636e-05
2075.0 6.051106040130968e-05
2080.0 6.326447626997097e-05
2085.0 6.60304287063465e-05
2090.0 6.880891771043627e-05
2095.0 7.159994328224026e-05
2100.0 7.440350542175852e-05
2105.0 7.745262372366961e-05
2110.0 8.051538557474235e-05
2115.0 8.359179097497673e-05
2120.0 8.668183992437276e-05
2125.0 8.978553242293042e-05
2130.0 9.290286847064974e-05
2135.0 9.60338480675307e-05
2140.0 9.917847121357329e-05
2145.0 0.00010233673790877756
2150.0 0.00010550864815314345
2155.0 0.00010869420194667097
2160.0 0.00011189339928936014
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2170.0 0.00011833272462222341
2175.0 0.00012157285261239751
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2185.0 0.00012809403924023065
2190.0 0.0001313750978778897
2195.0 0.00013466980006471039
2200.0 0.0001379781458006927
2205.0 0.00013697162005895603
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2215.0 0.00013494060786205768
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2305.0 0.00011709491260915991
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2905.0 0.0017136314040109434
2910.0 0.001683037129351848
2915.0 0.0016523275841556356
2920.0 0.001621502768422306
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2930.0 0.0015595073253442955
2935.0 0.0015283366979996146
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2960.0 0.0013707545032194506
2965.0 0.001338892252652066
2970.0 0.0013069147315475647
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3140.0 0.0018261874293952524
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3150.0 0.0019161645607432046
3155.0 0.001961353510340549
3160.0 0.00200667604922014
3165.0 0.002052132177381976
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3200.0 0.002374065574417713
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3210.0 0.0024188074700601065
3215.0 0.0024412656210138317
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Instrument/throughputs/u_throughput.txt 0 → 100644
View file @ b2540417
# u_cssc
# lambda_Angst throughput
2000.00 0.00000
2010.00 0.00000
2020.00 0.00000
2030.00 0.00000
2040.00 0.00000
2050.00 0.00000
2060.00 0.00000
2070.00 0.00000
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2090.00 0.00000
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2150.00 0.00000
2160.00 0.00000
2170.00 0.00000
2180.00 0.00000
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2200.00 0.00000
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2270.00 0.00000
2280.00 0.00000
2290.00 0.00000
2300.00 0.00000
2310.00 0.00000
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Instrument/throughputs/y_throughput.txt 0 → 100644
View file @ b2540417
# y_cssc
# lambda_Angst throughput
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10960.00 0.00090
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Instrument/throughputs/z_throughput.txt 0 → 100644
View file @ b2540417
# z_cssc
# lambda_Angst throughput
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View file @ b2540417
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R 0 → 100755
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StrayLight.cpp 0 → 100755
View file @ b2540417
// #include"StrayLight.h"
#include<iostream>
#include<string>
#include<fstream>
#include<cmath>
#include<string>
#include<ctime>
#include<iomanip>
#include<sstream>
#include<string.h>
#include"ephcom_wrapper.hpp"
using namespace std;
#define PI acos(-1)
#define Es 1367.0
#define Em 0.0044
#define Re 6371.0//地球半径
#define Re2 Re*Re
#define Swide 2.44//2023年4月1日结构设定为2.4425m，以后还可能变化，为方便计算设为2.44，不会有数量级误差
#define Slong 3.01//2023年4月1日结构设定为3.01m
#define Rd 1.1//2023年4月1日结构设定为1.128m，以后还可能变化，为方便计算设为1.1，不会有数量级误差
#define Plank 6.626e-34 //普朗克常数J*s
#define AU 149597870.7 //天文单位km
#define AU2 AU*AU
const double Es_fil[7] = {27.01477,86.82985,281.07176,255.6571,193.52574,200.77139,123.77403};
const double Em_fil[7] = {8.695317e-05,0.00027948159,0.0009046933,0.00082289045,0.00062290655,0.00064622833,0.00039839482};
const double PlanetsAbsMag[8][7]={2.231,0.782,-0.419,-0.773,-0.798,-0.718,-0.672,//水星
-3.367,-3.872,-4.410,-4.512,-4.398,-4.212,-4.117,//金星
1.130,0.101,-1.523,-2.520,-2.650,-2.503,-2.358,//火星
-8.528,-9.033,-9.402,-9.386,-9.047,-8.448,-8.421,//木星
-8.708,-9.213,-9.708,-9.764,-9.396,-8.608,-8.368,//土星
-6.346,-6.851,-7.197,-6.673,-5.336,-4.912,-5.317,//天王星
-5.933,-6.438,-6.900,-6.659,-5.470,-4.837,-5.081,//海王星
0.664,0.159,-0.719,-1.188,-1.196,-0.974,-0.891};//冥王星
const double EM0 = 2.8e-8;//0星等的照度值，公式：double E0 = 1365.08 / pow(100, 26.72 / 5);
//const double PlanetsAbsE[8][7]={3.58722e-09,1.36257e-08,4.11868e-08,5.70635e-08,5.83926e-08,5.42448e-08,5.19946e-08,
//6.2224e-07,9.90736e-07,1.62614e-06,1.78631e-06,1.60827e-06,1.35506e-06,1.24153e-06,
//9.88913e-09,2.55128e-08,1.13857e-07,2.85206e-07,3.21483e-07,2.80775e-07,2.45673e-07,
//7.21702e-05,0.00011491,0.00016142,0.000159059,0.000116401,6.70437e-05,6.5397e-05,
//8.5184e-05,0.000135631,0.000213973,0.000225298,0.000160531,7.76887e-05,6.22814e-05,
//9.67293e-06,1.54013e-05,2.11816e-05,1.30725e-05,3.81556e-06,2.58201e-06,3.74937e-06,
//6.61238e-06,1.05283e-05,1.61123e-05,1.2905e-05,4.31676e-06,2.40967e-06,3.01688e-06,
//1.519e-08,2.41857e-08,5.42948e-08,8.36292e-08,8.42477e-08,6.86686e-08,6.36148e-08};//水金火木土天海冥的绝对星等对应辐照度
const double PlanetsAbsE[8][7]={1.25183e-09,3.49052e-09,1.10171e-08,8.90266e-09,6.1621e-09,5.74084e-09,3.38622e-09,2.1714345e-07,2.5379912e-07,4.3497813e-07,2.7868908e-07,1.6971832e-07,1.4340872e-07,8.085651e-08,3.45101e-09,6.53567e-09,3.045562e-08,4.44959e-08,3.392569e-08,2.971499e-08,1.599982e-08,2.518527664e-05,2.94367667e-05,4.317848695e-05,2.481532382e-05,1.228368626e-05,7.0953786e-06,4.259072e-06,2.972670174e-05,3.474482318e-05,5.72357555e-05,3.514956436e-05,1.694059717e-05,8.22196406e-06,4.05615911e-06,3.37556695e-06,3.94539151e-06,5.66588062e-06,2.03948233e-06,4.0265094e-07,2.7325969e-07,2.4418275e-07,2.30752665e-06,2.69705688e-06,4.30990224e-06,2.0133531e-06,4.5554231e-07,2.5502078e-07,1.9647848e-07,5.30086e-09,6.1957e-09,1.452337e-08,1.304728e-08,8.89055e-09,7.26734e-09,4.143e-09};//水金火木土天海冥的绝对星等对应辐照度
const double PlanetsE_AU2[8][7]={28015446.582343537,78116167.85424984,246557514.80383125,199237356.53256097,137904849.78902856,128477299.08430137,75781955.27849847,4859566726.294486,5679903143.209061,9734602982.59355,6236928580.011572,3798214956.1848063,3209418842.794384,1809530078.5522048,77232047.71057059,146265173.2621918,681582206.1057857,995796902.2089956,759240802.5227964,665007277.5659081,358068244.0283927,563634475859.0736,658780794948.3726,966313938206.4478,555355108216.219,274903038143.9954,158791188059.1252,95315999534.81744,665269402821.2107,777572566648.6147,1280908901968.4758,786630481203.9672,379122482579.8927,184003633079.88455,90774905710.84904,75543577847.78088,88295979751.68683,126799705213.53505,45642641530.34039,9011135901.611265,6115421532.435761,5464693473.842928,51641345572.125656,60358846283.05587,96453556060.02104,45057881748.61057,10194819466.938034,5707243446.332199,4397094572.220029,118630824.75843115,138656722.37423745,325026105.3318717,291991877.7040579,198966307.20634192,162639637.65618783,92718373.92902023};//八个行星辐照度乘以一个天文单位的平方，便于事后计算实际场景辐照度
const double SunRatio[7] ={0.07209039,0.1050749,0.26816488,0.22462947,0.18818067,0.1100292,0.03183049};
const double MoonRatio[7]={0.07199216,0.10505516,0.26823942,0.22467527,0.18816909,0.11004074,0.03182816};
const int Planets[8]={MERCURY,VENUS,MARS,JUPITER,SATURN,URANUS,NEPTUNE,PLUTO};
extern "C"{
class XYZ//三维坐标类
{
public:
double X;
double Y;
double Z;
double Length;
XYZ()
{
X = Y = Z = Length = 0;
}
XYZ(double x, double y, double z)
{
X = x, Y = y, Z = z, Length = Model();
}
XYZ(double a[3])
{
X=a[0],Y=a[1],Z=a[2],Length=Model();
}
double Model()//模
{
return sqrt(X*X + Y*Y + Z*Z);
}
double Square()
{
return X*X + Y*Y + Z*Z;
}
double Cos(XYZ A)//夹角的cos值
{
return (X*A.X + Y*A.Y + Z*A.Z) / (Model()*A.Model());
}
double Angle(XYZ A)//夹角弧度
{
double a = X*A.X + Y*A.Y + Z*A.Z;
double b = Model()*A.Model();
double c = a / b;
if (c > 1)return 0;
else if (c < -1)return acos(-1);
else return acos(c);
}
double Azimuth(XYZ A, XYZ py)//方位夹角弧度
{
double coefficient = (X*A.X + Y*A.Y + Z*A.Z) / (X*X + Y*Y + Z*Z);
XYZ az = XYZ(A.X - X*coefficient, A.Y - Y*coefficient, A.Z - Z*coefficient);
double c = az.Cos(py);
return acos(c);
}
XYZ Cross(XYZ A)
{
return XYZ(Y*A.Z - Z*A.Y, Z*A.X - X*A.Z, X*A.Y - Y*A.X);
}
XYZ Normalize()
{
return XYZ(X / Length, Y / Length, Z / Length);
}
XYZ operator+(XYZ a)
{
return XYZ(X + a.X, Y + a.Y, Z + a.Z);
}
XYZ operator-(XYZ a)
{
return XYZ(X - a.X, Y - a.Y, Z - a.Z);
}
double operator*(XYZ a)
{
return X*a.X + Y*a.Y + Z*a.Z;
}
};
class YZ//二维坐标类
{
public:
double Y;
double Z;
YZ()
{
Y=Z=0;
}
YZ(double y,double z)
{
Y=y,Z=z;
}
double Model()//模
{
return sqrt(Y*Y+Z*Z);
}
double Square()
{
return Y*Y+Z*Z;
}
double Angle(YZ a)//夹角弧度
{
return acos((Y*a.Y+Z*a.Z)/(Model()*a.Model()));
}
};
void Init();
double PST(double Azimuth,double Angle);//73*45，行是方位角角5度一分，列是夹角2度一分，PST每个数占16字符，每行720+2字符
XYZ Spherical2Cartesian(double latitude,double longitude);//天球转三维，参数为弧度
void Cartesian2Spherical(XYZ car, double sph[2]);//所得sph是纬度经度的弧度
XYZ Ecliptic2Equatorial(XYZ Ecl);//黄道转赤道
XYZ Equatorial2Ecliptic(XYZ Equ);//赤道转黄道
double ShelterEarth(XYZ sat,XYZ star);//卫星是否会被地球遮挡
double ShelterPlate(XYZ sp,XYZ ob,XYZ py,double fai,double op,double sum);//亮星是否会被盖板遮挡
void PointSource(double jd, double sat[3], double ob[3], double py[3], double E[7]);
void EarthShine(double ju, double sat[3], double ob[3], double py[3], double E[7]);
void Zodiacal(double ju, double ob[3], double E[7]);//琢磨半晌形参还是用赤道坐标系吧，内部再转换黄道！
void Calculate(double ju, double sat[3], double ob[3], double py[3], double E[7]);
void ComposeY(double ob[3], double py1[3], double py2[3]);
void Watt2Photon(double E[7], double P[7]);//照度w/m2转光子数ph/(s*100um2)
double Pst[73][45];
const int Rrow = 180, Rcol = 288;
double R[Rrow][Rcol];
double ZL[37][19];
string de405("DE405");
Ephcom ephcom(de405);
void Init()
{
ifstream infile("PST");
string s;
for (int i = 0; i < 73; i++)
{
getline(infile, s);
stringstream ss(s);
for (int j = 0; j < 45; j++)
{
ss >> Pst[i][j];
}
}
infile.close();
infile.open("R");
for (int i = 0; i < Rrow; i++)
{
for (int j = 0; j < Rcol; j++)
{
infile >> R[i][j];
}
}
infile.close();
infile.open("Zodiacal");
for (int i = 0; i < 37; i++)
{
for (int j = 0; j < 19; j++)
{
infile >> ZL[i][j];
}
}
infile.close();
}
double PST(double Azimuth,double Angle)//73*45，行是方位角角5度一分，列是夹角2度一分，PST每个数占16字符，每行720+2字符
{
double daz=Azimuth*36/PI;
double dan=Angle*90/PI;
int az=daz;
int an=dan;
if(an==0)return 0;
double pst=Pst[az][an-1]*(az+1-daz)*(an+1-dan)+Pst[az][an]*(az+1-daz)*(dan-an)+Pst[az+1][an-1]*(daz-az)*(an+1-dan)+Pst[az+1][an]*(daz-az)*(dan-an);
return pst;
}
XYZ Spherical2Cartesian(double latitude,double longitude)//天球转三维，参数为弧度
{
return XYZ(cos(latitude)*cos(longitude),cos(latitude)*sin(longitude),sin(latitude));
}
void Cartesian2Spherical(XYZ car, double sph[2])//所得sph是纬度经度的弧度
{
sph[0] = asin(car.Z / car.Length);
sph[1] = acos(car.X / sqrt(car.X*car.X + car.Y*car.Y));
if (car.Y < 0)sph[1] = -sph[1];
}
XYZ Ecliptic2Equatorial(XYZ Ecl)//黄道转赤道
{
double cosa = 0.917392;
double sina =-0.397983;
return XYZ(Ecl.X,Ecl.Y * cosa + Ecl.Z * sina,-Ecl.Y * sina + Ecl.Z * cosa);
}
XYZ Equatorial2Ecliptic(XYZ Equ)//赤道转黄道
{
double cosa = 0.917392;
double sina = 0.397983;
return XYZ(Equ.X, Equ.Y * cosa + Equ.Z * sina, -Equ.Y * sina + Equ.Z * cosa);
}
double ShelterEarth(XYZ sat,XYZ star)//卫星是否会被地球遮挡
{
double angle=star.Angle(sat);
if(angle>PI/2)
{
double dis=sat.Model()*sin(angle);
if(dis<Re)
{
return 0;
}
else
{
return 1;
}
}
else
{
return 1;
}
}
double ShelterPlate(XYZ sp,XYZ ob,XYZ py,double fai,double op,double sum)//亮星是否会被盖板遮挡
{
double theta=sp.Angle(ob);
double faisp=ob.Azimuth(sp,py);
double faidiff=faisp-fai;
if(theta<op||abs(faidiff)>=PI/2)
{
return 1;
}
else
{
double a=cos(theta);
double b=sin(theta)*cos(faidiff);
double c=sin(theta)*sin(faidiff);
XYZ S=XYZ(a,b,c);
double sumin=0;
for(double y=-Rd; y<=Rd; y+=0.1)
{
for(double z=-sqrt(Rd*Rd-y*y); z<=sqrt(Rd*Rd-y*y); z+=0.1)
{
if((Slong*cos(op)-a/b*(Slong*sin(op)+Rd-y)>=0)&&(abs(z+(c*cos(op)*(Rd-y))/(b*cos(op)-a*sin(op)))<=Swide/2))
{
sumin++;
}
}
}
return 1-sumin/sum;
}
}
void PointSource(double ju, double sat[3], double ob[3], double py[3], double E[7])
{
XYZ SAT = XYZ(sat[0], sat[1], sat[2]);
XYZ OB = XYZ(ob[0], ob[1], ob[2]);
XYZ PY = XYZ(py[0], py[1], py[2]);
double pos[3], vel[3];
ephcom.getPosVel(SUN, ju, pos, vel);
XYZ sun = XYZ(pos[0], pos[1], pos[2]);
double thetasun = OB.Angle(sun);
if (thetasun < PI * 5 / 18)
{
cout << "观测方向与太阳夹角不可小于50度！目前只有" << thetasun * 180 / PI << "度！";
return;
}
double faisun = OB.Azimuth(sun, PY);
double fai, op;//盖板方位角，盖板打开角度-90°
if (thetasun >= PI * 5 / 18 && thetasun < PI * 65 / 180)
{
op = 15 * PI / 180;
fai = faisun;
}
else if (thetasun >= PI * 65 / 180 && thetasun < PI * 11 / 18)
{
op = 45 * PI / 180;
fai = faisun;
}
else
{
op = 45 * PI / 180;
fai = 0;
}
ephcom.getPosVel(MOON, ju, pos, vel);
XYZ moon = XYZ(pos[0], pos[1], pos[2]);
double thetamoon = OB.Angle(moon);
double faimoon = OB.Azimuth(moon, PY);
double moonphase = sun.Angle(moon) / PI;
double E1[7] = { 0, 0, 0, 0, 0, 0, 0 };
double pstsun, pstmoon;
if (thetasun <= PI / 2)
{
pstsun = pow(10, PST(faisun, thetasun));
}
else
{
pstsun = 0;
}
if (thetamoon <= PI / 2 && thetamoon >= PI / 90)
{
pstmoon = pow(10, PST(faimoon, thetamoon));
}
else
{
pstmoon = 0;
}
double sum = 411;
double Sheltersun, Sheltermoon;
Sheltersun = ShelterEarth(SAT, sun)*ShelterPlate(sun, OB, PY, fai, op, sum);
Sheltermoon = ShelterEarth(SAT, moon)*ShelterPlate(moon, OB, PY, fai, op, sum);
// double Esun = Es*pstsun*Sheltersun, Emoon = Em*pstmoon*moonphase*Sheltermoon;
for (int i = 0; i < 7; i++)
{
E1[i] = Es_fil[i]*pstsun*Sheltersun*SunRatio[i] + Em_fil[i]*pstmoon*moonphase*Sheltermoon*MoonRatio[i];
}
for (int i = 0; i < 2; i++)
{
ephcom.getPosVel(Planets[i], ju, pos, vel);
XYZ planet = XYZ(pos[0], pos[1], pos[2]);
double thetap = OB.Angle(planet);
if (abs(thetap) < 0.008726646259971648){
continue;
}
double faip = OB.Azimuth(planet, PY);
double pstp = pow(10, PST(faip, thetap));
double shelterp = ShelterEarth(SAT, planet)*ShelterPlate(planet, OB, PY, fai, op, sum);
double planetphase = sun.Angle(planet) / PI;
double proportion = pstp*shelterp*planetphase/planet.Square();
for (int j = 0; j < 7; j++)
{
E1[j] += PlanetsE_AU2[i][j] * proportion;
}
}
for (int i = 2; i < 8; i++)
{
ephcom.getPosVel(Planets[i], ju, pos, vel);
XYZ planet = XYZ(pos[0], pos[1], pos[2]);
double thetap = OB.Angle(planet);
if (abs(thetap) < 0.008726646259971648){
continue;
}
double faip = OB.Azimuth(planet, PY);
double pstp = pow(10, PST(faip, thetap));
double shelterp = ShelterEarth(SAT, planet)*ShelterPlate(planet, OB, PY, fai, op, sum);
double proportion = pstp*shelterp/planet.Square();
for (int j = 0; j < 7; j++)
{
E1[j] += PlanetsE_AU2[i][j] * proportion;
}
}
string s;
double Estar[7] = { 0, 0, 0, 0, 0, 0, 0 };
ifstream infile("BrightGaia_with_csst_mag");
while (getline(infile, s))
{
stringstream ss(s);
double x, y, z, d[7];
ss >> x;
ss >> y;
ss >> z;
for (int i = 0; i < 7; i++)
{
ss >> d[i];
}
XYZ star = XYZ(x, y, z);
double theta = OB.Angle(star);
if (abs(theta) < 0.008726646259971648){
continue;
}
if (theta<PI / 2 && theta>PI / 90)
{
double faistar = OB.Azimuth(star, PY);
double pst = pow(10, PST(faistar, theta));
double shelter = ShelterEarth(SAT, star)*ShelterPlate(star,OB,PY,fai,op,sum);//太费时间了
double proportion = pst*shelter;
for (int i = 0; i < 7; i++)
{
Estar[i] += d[i] * proportion;
}
}
}
infile.close();
// cout << "点源杂散光：";
for (int i = 0; i < 7; i++)
{
E[i] = E1[i] + Estar[i];
// cout << E[i] << " ";
}
// cout << endl;
}
void EarthShine(double ju, double sat[3], double ob[3], double py[3], double E[7])
{
XYZ SAT = XYZ(sat[0], sat[1], sat[2]);
XYZ OB = XYZ(ob[0], ob[1], ob[2]);
XYZ PY = XYZ(py[0], py[1], py[2]);
double pos[3], vel[3];
ephcom.getPosVel(SUN, ju, pos, vel);
XYZ sun = XYZ(pos[0], pos[1], pos[2]);
ephcom.getPosVel(MOON, ju, pos, vel);
XYZ moon = XYZ(pos[0], pos[1], pos[2]);
double moonphase = sun.Angle(moon) / PI;
double S[Rrow][Rcol];
double wd = -PI / 2, jd = -PI, dwd = PI / 180, djd = PI / 150;
double x[Rrow][Rcol], y[Rrow][Rcol], z[Rrow][Rcol], sunangle[Rrow][Rcol], moonangle[Rrow][Rcol];
double Ese[Rrow][Rcol], Eme[Rrow][Rcol], Ee[Rrow][Rcol];
for (int i = 0; i < Rrow; i++)
{
jd = -PI;
for (int j = 0; j < Rcol; j++)
{
S[i][j] = Re2*cos(wd)*dwd*djd;
x[i][j] = Re*cos(wd)*cos(jd);
y[i][j] = Re*cos(wd)*sin(jd);
z[i][j] = Re*sin(wd);
XYZ v = XYZ(x[i][j], y[i][j], z[i][j]);
sunangle[i][j] = v.Angle(sun);
moonangle[i][j] = v.Angle(moon);
if (sunangle[i][j] < PI / 2)
{
Ese[i][j] = Es*cos(sunangle[i][j])*R[i][j] * S[i][j];
Eme[i][j] = 0;
}
else
{
Ese[i][j] = 0;
if (moonangle[i][j] < PI / 2)
{
Eme[i][j] = Em*moonphase*cos(moonangle[i][j])*R[i][j] * S[i][j];
}
else
{
Eme[i][j] = 0;
}
}
Ee[i][j] = Ese[i][j] + Eme[i][j];
jd += djd;
}
wd += dwd;
}
double thetasun = OB.Angle(sun);
double faisun = OB.Azimuth(sun, PY);
double fai, op;
if (thetasun < PI * 5 / 18)
{
cout << "观测方向与太阳夹角不可小于50度！目前只有" << thetasun * 180 / PI << "度！";
return;
}
else if (thetasun >= PI * 5 / 18 && thetasun < PI * 65 / 180)
{
op = 15 * PI / 180;
fai = faisun;
}
else if (thetasun >= PI * 65 / 180 && thetasun < PI * 11 / 18)
{
op = 45 * PI / 180;
fai = faisun;
}
else
{
op = 45 * PI / 180;
fai = 0;
}
OB = OB.Normalize();
PY = PY.Normalize();
XYZ zccst = OB.Cross(PY);
XYZ sfa = XYZ(sin(op), -cos(op)*cos(fai), -cos(op)*sin(fai));//盖板法向量
double sw = -1.1, sl = 0.1, dlw = 0.2, dlw2 = 0.04;//盖板z轴、y轴坐标和小块长度、小块面积
int shieldW=Swide/dlw,shieldL=Slong/dlw;//盖板z轴\y轴方向，也就是宽\长方向，的小块数量；
double xs[shieldW][shieldL], ys[shieldW][shieldL], zs[shieldW][shieldL], Eshield[shieldW][shieldL];//盖板小块坐标和接收照度
double Rd2 = Rd*Rd;
for (int w = 0; w < shieldW; w++)
{
for (int l = 0; l < shieldL; l++)
{
Eshield[w][l] = 0;
}
}
for (int i = 0; i < Rrow; i++)
{
for (int j = 0; j < Rcol; j++)
{
XYZ v = XYZ(x[i][j] - SAT.X, y[i][j] - SAT.Y, z[i][j] - SAT.Z);//设施到地块
if (XYZ(x[i][j], y[i][j], z[i][j])*v < 0)//判断地块是否为地球本身遮挡
{
XYZ vp = XYZ(v*OB, v*PY, v*zccst);//设施到地块转化为设施坐标系
double Rv = v.Model();//设施到地块距离
double Rv2 = v.Square();
double coses = sfa*vp / Rv;//俩向量夹角的cos
if (coses > 0)
{
sw = -1.1;
for (int w = 0; w < shieldW; w++)
{
sl = 0.1;
for (int l = 0; l<shieldL; l++)
{
double y0 = Rd + sl*sin(op);
double z0 = sw;
double R0 = sqrt(y0*y0 + z0*z0);
double fai0 = asin(z0 / R0);
xs[w][l] = sl*cos(op);
ys[w][l] = R0*cos(fai0 + fai);
zs[w][l] = R0*sin(fai0 + fai);
double yjd = ys[w][l] - xs[w][l] * vp.Y / vp.X;
double zjd = zs[w][l] - xs[w][l] * vp.Z / vp.X;
if (yjd*yjd + zjd*zjd>Rd2)
{
Eshield[w][l] += Ee[i][j] * coses*dlw2 / 2 / PI / Rv2;
}
sl += dlw;
}
sw += dlw;
}
}
}
}
}
double dlr = 0.1, dlt = 0.5*PI;//镜筒分块的半径和角度差
int Mrow=Rd/dlr,Mcol=2*PI/dlt;
double ye[Mrow][Mcol], ze[Mrow][Mcol];//镜筒分块的y坐标和z坐标，x必为0,故可省略
double SM[Mrow][Mcol];//镜筒每个小块的面积
double Econe[Mrow][Mcol];
double Ealbedo1 = 0, Ealbedo2 = 0;//盖板反射进的地气光，直接射入的地气光
for (int i = 0; i < Mrow; i++)
{
for (int j = 0; j < Mcol; j++)
{
ye[i][j] = dlr*(i+0.5)*cos(dlt*j);
ze[i][j] = dlr*(i+0.5)*sin(dlt*j);
SM[i][j]=dlr*(i+0.5)*dlt*dlr;//分块中心弧长乘以分块半径，约等于梯形面积
Econe[i][j]=0;
for (int w = 0; w < shieldW; w++)
{
for (int l = 0; l < shieldL; l++)
{
XYZ ves = XYZ(xs[w][l], ys[w][l] - ye[i][j], zs[w][l] - ze[i][j]);//镜头分块到盖板小块
double tyj = acos(ves.X / ves.Length);
double fwj = acos(ves.Y / (sqrt(ves.Y*ves.Y + ves.Z*ves.Z)));
double ppp = pow(10, PST(fwj, tyj));
Econe[i][j] += Eshield[w][l] / 2 / PI / ves.Square()*0.03*pow(10, PST(fwj, tyj));
}
}
Econe[i][j]*=SM[i][j];
Ealbedo1+=Econe[i][j];
}
}
Ealbedo1=Ealbedo1/Rd2/PI;
for (int i = 0; i < Rrow; i++)
{
for (int j = 0; j < Rcol; j++)
{
XYZ v = XYZ(x[i][j] - SAT.X, y[i][j] - SAT.Y, z[i][j] - SAT.Z);//设施到地块
double earthangle = OB.Angle(v);//观测方向与设施到地块方向的夹角
double faie = OB.Azimuth(v, PY);//观测方向与设施到地块方向的方位角
if (earthangle < PI / 2 && XYZ(x[i][j], y[i][j], z[i][j])*v < 0)
{
double faie2 = faie - fai;
if (earthangle < op || abs(faie2)>PI / 2)
{
Ealbedo2 += pow(10, PST(faie, earthangle))*Ee[i][j] / 2 / PI / v.Square();
}
else
{
double D = 39961, J = 0;
for (double yn = -Rd; yn < Rd; yn += 0.01)
{
for (double zn = -Rd; zn < Rd; zn += 0.01)
{
if (yn*yn + zn*zn < Rd2)
{
double a = cos(earthangle);
double b = sin(earthangle)*cos(faie2);
double c = sin(earthangle)*sin(faie2);
if ((Slong*cos(op) >= a / b*(Slong*sin(op) - yn + Rd)) && (abs(zn + c*cos(op)*(zn - Rd) / (a*sin(op) - b*cos(op))) <= Swide / 2))
{
J++;
}
}
}
}
Ealbedo2 += pow(10, PST(faie, earthangle))*Ee[i][j] / 2 / PI / v.Square()*(1 - J / D);
}
}
}
}
double Ealbedo = Ealbedo1 + Ealbedo2;
// cout << "地气杂散光：";
for (int i = 0; i < 7; i++)
{
E[i] = Ealbedo*SunRatio[i];
// cout << E[i] << " ";
}
// cout << endl;
}
void Zodiacal(double ju, double ob[3], double E[7])
{
XYZ OB = XYZ(ob[0], ob[1], ob[2]);
double pos[3], vel[3];
ephcom.getPosVel(SUN, ju, pos, vel);
XYZ sun = XYZ(pos[0], pos[1], pos[2]);
double sph[2];
OB = Equatorial2Ecliptic(OB);
Cartesian2Spherical(OB, sph);
double latitude = sph[0] / PI * 180, longitude = sph[1] / PI * 180;
sun = Equatorial2Ecliptic(sun);
Cartesian2Spherical(sun, sph);
latitude = abs(latitude);
longitude -= sph[1] / PI * 180;
longitude = abs(longitude);
if (longitude > 180)longitude = 360 - longitude;
int lo, la;
double lor, lar;
lo = longitude / 5;
lor = longitude / 5.0 - lo;
la = latitude / 5;
lar = latitude / 5.0 - la;
double zl = ZL[lo][la] * (1 - lor)*(1 - lar) + ZL[lo][la + 1] * (1 - lor)*lar + ZL[lo + 1][la] * lor*(1 - lar) + ZL[lo + 1][la + 1] * lor*lar;
zl*=PI / 784 * 1e-11;
double u[7]= {132.3,106.944,110.541,43.8336,19.3065,6.54026,1.5624};
// cout << "黄道弥散光：";
for(int i=0; i<7; i++)
{
E[i]=zl*u[i];
// cout << E[i] << " ";
}
// cout << endl;
}
void Calculate(double ju, double sat[3], double ob[3], double py[3], double E[7])
{
double Ep[7],Ee[7],Ez[7];
PointSource(ju, sat,ob,py,Ep);
EarthShine(ju, sat,ob,py,Ee);
Zodiacal(ju,ob,Ez);
// cout << "总杂散光：";
for(int i=0; i<7; i++)
{
E[i]=Ep[i]+Ee[i]+Ez[i];
// cout<<E[i]<<" ";
}
// cout << endl;
}
void ComposeY(double ob[3], double py1[3], double py2[3])
{
XYZ OB=XYZ(ob);
XYZ Eclob = Equatorial2Ecliptic(OB);
double sph[2];
Cartesian2Spherical(Eclob, sph);
if (abs(abs(sph[0]) - PI / 2) < 1e-6)
{
cout << "光轴不可指向极点";
return;
}
double decy1 = sph[0] + PI / 2, decy2 = sph[0] - PI / 2;
double ray1, ray2;
if (decy1 > PI / 2)
{
decy1 = PI - decy1;
ray1 = sph[1] + PI;
}
else ray1 = sph[1];
if (decy2 > -PI / 2)ray2 = sph[1];
else
{
decy2 = -decy2 - PI;
ray2 = sph[1] + PI;
}
XYZ eclpy1 = Spherical2Cartesian(decy1, ray1);
XYZ eclpy2 = Spherical2Cartesian(decy2, ray2);
XYZ PY1 = Ecliptic2Equatorial(eclpy1);
XYZ PY2 = Ecliptic2Equatorial(eclpy2);
py1[0]=PY1.X,py1[1]=PY1.Y,py1[2]=PY1.Z;
py2[0]=PY2.X,py2[1]=PY2.Y,py2[2]=PY2.Z;
}
void Watt2Photon(double E[7], double P[7])//照度w/m2转光子数ph/(s*100um2)
{
double c = 3e8;
double lamda[7]= {275e-9,354e-9,475e-9,622e-9,763e-9,900e-9,990e-9};
double co=1e-10/Plank/c;//m2到100um2的系数
//cout << "各谱段在单个像元的光子数：";
for(int i=0; i<7; i++)
{
P[i]=E[i]*lamda[i]*co;
//cout<<P[i]<<" ";
}
//cout << endl;
}
void Zodiacal1(double lonlat[2], double E[7])
{
double latitude = abs(lonlat[1]);
double longitude = abs(lonlat[0]);
if (longitude > 180)longitude = 360 - longitude;
int lo, la;
double lor, lar;
lo = longitude / 5;
lor = longitude / 5.0 - lo;
la = latitude / 5;
lar = latitude / 5.0 - la;
double zl = ZL[lo][la] * (1 - lor)*(1 - lar) + ZL[lo][la + 1] * (1 - lor)*lar + ZL[lo + 1][la] * lor*(1 - lar) + ZL[lo + 1][la + 1] * lor*lar;
zl*=PI / 784 * 1e-11;
double u[7]={132.3,106.944,110.541,43.8336,19.3065,6.54026,1.5624};
// cout << "黄道弥散光：";
for(int i=0;i<7;i++)
{
E[i]=zl*u[i];
// cout << E[i] << " ";
}
// cout << endl;
}
}
Zodiacal 0 → 100755
View file @ b2540417
30000 15000 7000 3140 1610 985 640 439.106795917950 332.953759944373 275 227.040718244473 184.215493793075 150 126.619219993047 111.295375994437 100 88.7046240055627 73.3807800069534 50
20000 12000 6000 2940 1540 945 625 434.136797758554 329.872405260036 271 223.547334192282 182.480458923860 150 127.340532138986 111.872425711189 100 88.1275742888112 72.6594678610140 50
16000 8000 4740 2470 1370 865 590 424.924281880506 325.703844589420 264 216.192536238306 177.535146441613 148 127.046313907011 112.081495570053 100 87.6962822077246 72.0647972041002 50.0000000000000
11500 6780 3440 1860 1110 755 525 379.404487437312 298.581196755993 251 210.819373149455 174.952207929139 146 125.577279224129 111.350712268192 100 88.2048432873637 72.6449429980935 50
6400 4480 2410 1410 910 635 454 340.751783794961 276.748855303552 237 201.241198619320 168.117212939671 141 122.135273579611 109.263774419244 99 87.9584478029781 72.7536153092783 50
3840 2830 1730 1100 749 545 410 320.344426947347 262.847445764680 223 188.949910583017 159.472507970269 136 119.263338127992 107.188448280172 97 85.9226628309394 71.1811063164520 50
2480 1870 1220 845 615 467 365 293.396992658036 243.591181463075 207 176.533897785140 151.075388060617 131 116.245193979181 104.996155183345 95 84.0038448166554 69.7548060208193 50
1650 1270 910 680 510 397 320 264.610999197860 224.242861979717 193 166.095447800706 143.176731474096 125 111.822024414131 101.902063975749 93 82.8757138020283 69.2890866969798 50
1180 940 700 530 416 338 282 239.383076216900 206.105287077371 179 155.528255539422 135.661786794464 120 108.689086810597 100.062380559589 92 82.3820638848555 69.0886909671804 50
910 730 555 442 356 292 250 217.177087096913 189.491057165516 166 145.936910467127 129.234403723928 116 106.038233997541 97.9416983091442 90 80.5027461353003 67.7395437802365 50
727.458461874842 590.813948067450 458.193770946183 380.572133876131 310.356532547090 256.488736025072 222.994441816550 196.671226703445 173.815072589959 153.993110811782 136.873310808416 122.526994434613 111.126321648939 102.546129456415 95.4719630478941 88.2920446606834 79.3945965320918 67.1678408994278 50
597.965786285821 501.989953285938 394.904124012041 330.741575203306 272.426631477206 229.377054599373 200.722233330368 178.298184971317 159.500061954463 143.183118953515 128.502453511432 115.812534648182 105.767674252986 98.6162295599359 92.9827391826220 87.0857870795079 79.1439572090571 67.3758335297333 50
505 442 352 292 243 209 183 162.948572168708 147.332365312119 134 121.348535356634 109.968784724353 101 95.0646938121630 90.7184217163971 86 78.9482449502696 67.6019728545037 50
434.185639242502 392.917767644504 318.376629582089 263.460345936839 222.213128168793 193.706429839947 169.485130042169 151.204192642909 137.846384427846 126.706631884706 115.748672194896 105.611485314551 97.6028618934907 92.4866702185601 88.8510891247191 84.7403750839550 78.1987845682555 67.2705740496079 50
379.733278070694 351.223716015657 291.034402908743 242.720597293047 207.589653411575 181.900455075790 159.198062706301 142.411627057649 130.568767913886 120.897501975771 111.291656158755 102.308298237053 95.1703061995698 90.5932607902020 87.2635537728093 83.3602796662423 77.0625329893514 66.5494082609872 50
338 317 269 227 196 172 151 135.608650155770 124.774226094307 116 107.379198451166 99.3648656018433 93 88.8745560395662 85.7663114983196 82 75.9003551683471 65.7921106271005 50
305.576758932926 289.996462836015 251.299710725463 213.919815709849 184.976139962921 162.759618689212 143.916889866626 129.942315002235 119.830751582977 111.550732019764 103.559236179535 96.2670337533281 90.5733418882097 86.9591551723739 84.2325779585342 80.7834920405337 75.0017792122157 65.2773212674234 50
279.989990320293 268.633701169951 236.958264352989 202.709368957841 174.696236357976 154.280384356725 137.633663992575 124.996787950500 115.479466152946 107.523169439697 99.9646100690791 93.2214659735947 88.1066565042906 85.0296921673207 82.7864480892672 79.7693905518192 74.3709858366659 64.9837002254965 50
259 251 225 193 166 147 132 120.465513676140 111.554773867063 104 96.8743867494711 90.6150297791503 86 83.4073096963458 81.6147366459656 79 73.9408189095900 64.8149125258764 50
240.766584285053 235.503788418843 214.572675664209 184.452983816359 159.437867535078 141.218058366167 126.921384565401 116.141066332417 107.932382590812 101.016365962164 94.4576243640234 88.6950668978497 84.5111779610779 82.2885391283921 80.8101206834713 78.4589900872436 73.6182148006372 64.6708622845800 50
225.047501388876 221.834071897130 205.317724864488 176.849334282997 154.403178934298 136.681711201015 122.526540582659 112.212537983324 104.653215400233 98.4172276728472 92.4433471106159 87.1508159029366 83.3289937091939 81.3714666204164 80.0887264542075 77.8954914598142 73.2064798864838 64.4364099834633 50
212 210 197 170 150 133 119 108.968150170540 101.799499174001 96 90.4505707007701 85.5319895790017 82 80.2295670263797 79.0725425099927 77 72.4830130455629 63.9926551958425 50
201.690237260197 200.025420525649 189.446623654739 163.786767543232 145.568686193063 129.849629327603 116.434608908807 106.594275830766 99.4340907887345 93.6430633908398 88.2383060221020 83.5493421751065 80.2337981193304 78.5974046590145 77.5383107374556 75.6027698327141 71.3370354228506 63.2873609859257 50
193.820004124204 191.992974204493 182.733799152023 158.374775391654 141.394751608534 127.177956024402 114.556469973086 104.869893480803 97.5423671128237 91.5486606096547 86.1255446666051 81.5577937981954 78.3921834737485 76.8539016661414 75.8817863624661 74.0930880533685 70.1050572294944 62.5349443814896 50
188 186 177 154 138 125 113 103.472133032474 96.0903350126002 90 84.5712734023673 80.0733060196831 77 75.5390696543528 74.6534779457045 73 69.2354109431844 62.0164859012028 50
183.842837044530 182.024159108189 172.344533420539 150.807353418120 135.768869174150 123.346387286385 111.525364984557 102.194863876581 95.0804127903208 89.2261952892916 83.9273482154446 79.4828215244692 76.4425184504893 75.0392867782103 74.2377524946620 72.6854861374556 69.0300582442024 61.9190393525135 50
180.968778410604 179.564401655269 168.710041490384 148.577490076315 134.536333150083 122.310168405082 110.395727673146 101.298913319835 94.6606644919416 89.2399817403860 84.1171019637652 79.6572074513917 76.5467168402564 75.1263973841518 74.3544108040747 72.8432674378230 69.2054776231947 62.0535516979877 50
179 178 166 147 134 122 110 101.161848147921 95.0155655993437 90 84.9567367232255 80.3383120527731 77 75.4186123665846 74.5571121154899 73 69.3317767733990 62.1369431889709 50
177.716192339462 176.914980078633 164.212279700143 145.946781747252 133.985466739967 122.542599304634 110.686153375186 102.107114286080 96.2902104428977 91.4521554519937 86.2753467707504 81.3049172606660 77.5516836342678 75.6227629219776 74.5104734257943 72.8034337656115 69.0902625613226 61.9595784328209 50
177.527104455602 176.712382137394 163.722331182737 146.018968006791 134.830286161505 124.136925910825 112.638397112107 104.241674217759 98.4721687469323 93.4914124288013 87.9535951873799 82.4835397260425 78.1987269430036 75.8001614550468 74.3229427532328 72.3856940471913 68.6070385465521 61.6055994609451 50
179 178 165 148 137 127 116 107.618369565958 101.509629084266 96 89.8850372551827 83.8376297796048 79 76.1007406725702 74.2139258713895 72 68.1194074619438 61.2325926607631 50
182.588689893918 181.204809466168 168.324866297409 152.368482555836 140.770745347464 131.186919198783 120.730021514699 112.131318192577 105.251463102523 98.8170347545853 91.9445480061505 85.3102631039541 79.9803766420691 76.6271017220435 74.3467174753257 71.8415195408390 67.8138035575069 60.9658651642528 50
188.293174137357 186.030514239601 173.215448593483 158.383674933557 145.661040722416 136.105090914582 126.050683878426 117.039742915109 109.149274748558 101.609183359224 93.9322814719671 86.7630167892887 81.0287457580997 77.2925195138329 74.6601679460091 71.8732156326712 67.6731871518618 60.8016070816238 50
196 192 179 165 151 141 131 121.444142789946 112.555351044031 104 95.6297114342393 88.0370932777062 82 77.9629373990224 75.0370165858846 72 67.6296500807821 60.7037292676442 50
205.595714751532 198.636152427066 185.006773628739 171.171880621998 156.116737055362 145.117131307640 134.615982788241 124.445016873482 114.821979010604 105.613038862998 96.8183116745740 88.9736950113039 82.7490320196781 78.5042987286960 75.3600026973967 72.1267843673288 67.6152841800409 60.6361425770818 50
216.966865661637 205.461857200499 190.564022591480 175.853739666387 160.340365763647 147.701969690105 135.936645151968 125.142864222108 115.301445669936 106.071854134304 97.2795559745780 89.4140244321794 83.1307344690420 78.7825468539377 75.5118655829902 72.1584804591610 67.5621812854119 60.5627578647043 50
230 212 195 178 163 148 134 122.638183892218 113.346038043688 105 96.7949181158581 89.1992839824302 83 78.6636251258314 75.3753445451096 72 67.4024332326682 60.4474859852797 50
\ No newline at end of file
ephcom.c 0 → 100755
View file @ b2540417
//! @file
//! Source code for the ephcom library.
//!
// Copyright (C) 1994-2004 Paul Hardy
// Copyright (C) 2011 Alan W. Irwin
//
// This file is part of the timeephem software project.
//
// timeephem is free software; you can redistribute it and/or modify
// it under the terms of the GNU Library General Public License as published
// by the Free Software Foundation; version 2 of the License.
//
// timeephem is distributed in the hope that it will be useful,
// but WITHOUT ANY WARRANTY; without even the implied warranty of
// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
// GNU Library General Public License for more details.
//
// You should have received a copy of the GNU Library General Public License
// along with timeephem; if not, write to the Free Software
// Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301 USA
// Note that this software is not a product of the Jet Propulsion
// Laboratory; it just uses and supports their ASCII and binary
// ephemeris files. Please don't mail JPL concerning any bugs.
// Send bug reports or suggestions to airwin@users.sourceforge.net instead.
//
// This file contains the following routines. Running "make test" will
// check the proper operation of every one of these routines.
//
// ephcom_readascii_header() - read ASCII header file
// ephcom_readascii_block() - read ASCII coefficient block
// ephcom_readbinary_header() - read header from binary ephemeris
// ephcom_readbinary_block() - read coefficient block from binary
// ephemeris
// ephcom_writeascii_header() - write header in ASCII
// ephcom_writeascii_block() - write coefficient block in ASCII
// ephcom_writebinary_header() - write header to binary ephemeris file
// ephcom_writebinary_block() - write coefficient block to binary
// ephemeris file
// ephcom_parse_block() - parse ("pretty print") a coefficient block
// ephcom_nxtgrp() - read next "GROUP" from ASCII header
// ephcom_outdouble() - write byte-swapped double to a file
// ephcom_outint() - write byte-swapped int to a file
// ephcom_indouble() - read byte-swapped double from a file
// ephcom_inint() - read byte-swapped int from a file
// ephcom_doublstrc2f() - change C ASCII double string to FORTRAN
// [there is no corresponding
// ephcom_doublestrf2c() routine;
// for FORTRAN to C format conversion,
// just change FORTRAN's double precision
// 'D' exponent to 'E' in your software
// and everything else should parse fine]
// ephcom_pleph() - calculate <x,y,z> and <xdot,ydot,zdot>
// for a given target and center, AFTER
// calling ephcom_get_coords() (different
// sequence than with JPL's FORTRAN PLEPH)
// ephcom_get_coords() - calculate <x,y,z> and <xdot,ydot,zdot>
// for all Solar System objects at a
// given time
// ephcom_cheby() - interpolates Chebyshev coefficients
// for one sub-block of coefficients
// for one Solar System object at a
// given time
// ephcom_jd2cal() - convert Julian Day to Julian or Gregorian
// Year, Month, Day, Hour, Minute, Second
// ephcom_cal2jd() - convert Julian or Gregorian calendar
// Year, Month, Day, Hour, Minute, Second
// to Julian Day
//
// The indouble() and outdouble() routines rely upon the gnulliver64c()
// routine from gnulliver.c.
//
// The inint() and outint() routines rely upon the gnulliver32() routine
// from gnulliver.c.
//
//
#include <stdio.h>
#include <stdlib.h>
#include <ctype.h>
#include <string.h>
#include <math.h> // IF_SAME_DATE macro uses fabs, ephcom_split uses modf.
#include "ephcom.h"
#include "gnulliver.h"
// Declare static functions.
static void
ephcom_nxtgrp( char *group, const char *expected, FILE *infile );
static void
ephcom_outdouble( FILE *outfp, double x );
static void
ephcom_outint( FILE * outfp, unsigned u );
static void
ephcom_doublestrc2f( char *buf );
static double
ephcom_exact_time( double time );
static double
ephcom_split( double time, double * itime );
// ephcom_cheby() - interpolate at a point using Chebyshev coefficients.
static inline void
ephcom_cheby( int maxcoeffs, double x, double span, double *y,
int ncoords, int ncoeffs, double *pv );
//
// ephcom_jd2cal() - convert Julian Day to calendar date and time.
//
// tjd: double precision Julian Day
// idate: integer year, month, day, hour, minute, second of tjd
// calendar_type: -1=Julian; 0=Automatic; 1=Gregorian
//
// If automatic, use Julian calendar for dates before 15 October 1582.
//
// From pp. 604, 606 in the Explanatory Supplement to the Astronomical Almanac.
//
static void
ephcom_jd2cal( double tjd, int idate[6], int calendar_type );
// Start of function definitions.
//! Read a JPL ephemeris ASCII header from the FILE pointed to by the
//! infp argument and store all header data in the ephcom_Header
//! struct pointed to by the header argument. If any errors are
//! detected this routine writes a message to stderr and exits.
//!
//! @param infp [IN ONLY]Pointer to an ascii version of a JPL
//! ephemeris FILE.
//! @param header [OUT ONLY]Pointer to an ephcom_Header struct which
//! upon return will contain all the JPL ephemeris header information
//! that has been read from the FILE.
//!
void
ephcom_readascii_header( FILE * infp, ephcom_Header *header )
{
char group[13]; // To store the "GROUP" header line information
double val1, val2, val3; // To read text line with 3 double precision words
int i, j, k, n;
int iword; // word number we're reading in a line
int blockout; // number of bytes we've written to current block/rec in file
int blockbytes; // number of bytes in a block, equals 8 * ncoeff
char readbuf[EPHCOM_MAXLINE + 1];
char outhcars[EPHCOM_MAXLINE + 1];
size_t fwrite( const void *ptr, size_t size, size_t nmemb, FILE *stream );
//
// First header line: KSIZE= # NCOEFF= #
//
if ( infp != stdin )
rewind( infp );
fgets( readbuf, EPHCOM_MAXLINE, infp );
sscanf( readbuf, "%*6s%6d%*11s%6d", &header->ksize, &header->ncoeff );
blockbytes = 8 * header->ncoeff; // The size of a double, times # of doubles/block
if ( header->ksize != 2 * header->ncoeff )
{
fprintf( stderr, "Badly formed header; header->ksize != 2*header->ncoeff\n\n" );
exit( 1 );
}
//
// GROUP 1010: Title of ephemeris (DE/LE number, start JD, end JD)
//
//
// Blank all of header->ttl. Note that three fgets below
// only defines part of ttl so this blanking keeps valgrind
// quiet for subsequent accesses to all of ttl.
//
for ( i = 0; i < 3; i++ )
{
for ( j = 0; j < EPHCOM_MAXTTL; j++ )
header->ttl[i][j] = ' ';
header->ttl[i][EPHCOM_MAXTTL] = '\0';
}
ephcom_nxtgrp( group, "GROUP 1010", infp );
fgets( header->ttl[0], EPHCOM_MAXTTL + 2, infp ); // JPL Ephemeris title line
if ( strncmp( header->ttl[0], "JPL ", 4 ) != 0 )
{
fprintf( stderr, "\nERROR: file is not a JPL ASCII header file.\n\n" );
exit( 1 );
}
fgets( header->ttl[1], EPHCOM_MAXTTL + 2, infp ); // Start epoch
fgets( header->ttl[2], EPHCOM_MAXTTL + 2, infp ); // Finish epoch
//
// Convert any newlines or tabs to single spaces.
//
for ( i = 0; i < 3; i++ )
{
for ( j = 0; j < EPHCOM_MAXTTL; j++ )
if ( isspace( header->ttl[i][j] ) )
header->ttl[i][j] = ' ';
header->ttl[i][EPHCOM_MAXTTL] = '\0';
}
//
// GROUP 1030: Start and End JD, timestep (in JD) per block.
//
ephcom_nxtgrp( group, "GROUP 1030", infp );
fgets( readbuf, EPHCOM_MAXLINE, infp );
sscanf( readbuf, " %lE %lE %lE", &header->ss[0], &header->ss[1], &header->ss[2] );
//
// GROUP 1040: Constant names.
//
ephcom_nxtgrp( group, "GROUP 1040", infp );
fgets( readbuf, EPHCOM_MAXLINE, infp );
header->ncon = atoi( readbuf );
//
// Now read the constant names, 10 per line, each 6 characters long
// preceded by 2 blanks. Pad names with blanks to make 6 characters.
//
for ( i = 0; i < header->ncon; )
{
fgets( readbuf, EPHCOM_MAXLINE, infp );
if ( ( j = strlen( readbuf ) ) < 81 ) // Pad end with blanks for copying
{
// initial j is such a value that readbuf[j-1] is '\n'
while ( j < 81 )
readbuf[j++ - 1] = ' ';
readbuf[80] = '\n';
readbuf[81] = '\0';
}
for ( iword = 0; iword < 10 && i < header->ncon; iword++, i++ )
{
strncpy( header->cnam[i], &readbuf[2 + iword * 8], 6 );
header->cnam[i][6] = '\0';
}
}
//
// GROUP 1041: Constant values.
//
ephcom_nxtgrp( group, "GROUP 1041", infp );
fgets( readbuf, EPHCOM_MAXLINE, infp );
header->nval = atoi( readbuf );
if ( header->nval != header->ncon )
{
fprintf( stderr, "Error: number of constants and values not equal.\n\n" );
exit( 1 );
}
//
// Now read constant values, 3 per line, 26 characters each.
//
for ( i = 0; i < header->ncon; i += 3 )
{
fgets( readbuf, EPHCOM_MAXLINE, infp );
for ( j = 0; j < strlen( readbuf ); j++ )
if ( tolower( readbuf[j] ) == 'd' )
readbuf[j] = 'E';
// exponent is 'E'
sscanf( readbuf, "%lE %lE %lE",
&header->cval[i], &header->cval[i + 1], &header->cval[i + 2] );
}
//
// GROUP 1050: Constant values.
//
ephcom_nxtgrp( group, "GROUP 1050", infp );
for ( i = 0; i < 3; i++ )
{
fgets( readbuf, EPHCOM_MAXLINE, infp ); // Read line of 13 6-digit integers
for ( j = 0; j < 12; j++ )
{
header->ipt[j][i] = atoi( &readbuf[6 * j] );
}
header->lpt[i] = atoi( &readbuf[6 * 12] );
}
//
// If there are no coefficients for an ipt[i][] object (i.e., ipt[i][1]==0),
// then ipt[i][0] should contain the value of the next available coefficient
// number rather than 0, as per communication of Myles Standish to Paul Hardy
// on preferred format of ephemeris headers.
//
// If there are no libration coefficients (i.e., lpt[1]==0), then lpt[0]
// should contain the value of the next available coefficient number rather
// than 0 as well, as per the same communication from Myles Standish.
//
// First set j to maximum index into ipt[] that has coefficients
j = 0;
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][1] > 0 && header->ipt[i][0] > j )
j = i;
// Now set j to next available index count.
if ( header->lpt[1] > 0 && header->lpt[0] > j )
j = header->lpt[1] + header->lpt[1] * header->lpt[2] * 3;
else
j = header->ipt[j][0] +
header->ipt[j][1] * header->ipt[j][2] * ( j == 11 ? 2 : 3 );
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][0] == 0 )
header->ipt[i][0] = j;
if ( header->lpt[0] == 0 )
header->lpt[0] = j;
//
// Set the maximum number of Chebyshev coefficients possible for this file,
// to initialize position and velocity Chebyshev coefficient arrays during
// Chebyshev interpolation.
//
header->maxcheby = 0;
for ( i = 0; i < 12; i++ )
if ( header->ipt[i][1] > header->maxcheby )
header->maxcheby = header->ipt[i][1];
if ( header->lpt[1] > header->maxcheby )
header->maxcheby = header->lpt[1];
header->au = 0.0;
header->emrat = 0.0;
header->numde = 0;
for ( i = 0; i < header->ncon; i++ )
{
if ( strncmp( header->cnam[i], "AU ", 6 ) == 0 )
header->au = header->cval[i];
else if ( strncmp( header->cnam[i], "EMRAT ", 6 ) == 0 )
header->emrat = header->cval[i];
else if ( strncmp( header->cnam[i], "DENUM ", 6 ) == 0 )
header->numde = header->cval[i];
else if ( strncmp( header->cnam[i], "CLIGHT", 6 ) == 0 )
header->clight = header->cval[i];
else if ( strncmp( header->cnam[i], "LENUM ", 6 ) == 0 )
header->numle = header->cval[i];
}
if ( header->numle == 0 )
header->numle = header->numde;
//
// GROUP 1070: Constant values.
//
ephcom_nxtgrp( group, "GROUP 1070", infp );
//
// Now we're pointing to the first block of coefficient data, after header.
// Return at the point where we can start reading coefficients.
//
}
//! Read a block of data coefficients from a JPL ASCII ephemeris file.
//!
//! @param infp [IN ONLY]Pointer to an ascii version of a JPL
//! ephemeris FILE.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information that has already
//! been read from the FILE.
//! @param datablock [OUT ONLY]Pointer to an array that upon
//! successful return will be filled with datapoints == header->ncoeff
//! data points.
//! @returns number of coefficients read or 0 at EOF or some other i/o
//! error.
//!
int
ephcom_readascii_block(
FILE * infp,
ephcom_Header *header,
double *datablock )
{
int i, j;
int datalines; // lines of data we've read
int datapoints; // points of data we've read/converted/written
char readbuf[EPHCOM_MAXLINE + 1];
double val1, val2, val3; // To read text line with 3 double precision words
//
// First line in an ASCII block will be the block number, followed by
// the number of coefficients.
//
datalines = 0; // Not reported, but leave in for debugging
datapoints = 0;
if ( fgets( readbuf, EPHCOM_MAXLINE, infp ) && !feof( infp ) )
{
sscanf( readbuf, "%d %d", &i, &j );
if ( j != header->ncoeff )
{
fprintf( stderr,
"\nERROR: ASCII data file's %d coefficients/block\n", j );
fprintf( stderr,
" doesn't match ASCII header's %d coefficients/block.\n\n",
header->ncoeff );
exit( 1 );
}
datalines++;
while ( datapoints < header->ncoeff && !feof( infp ) )
{
fgets( readbuf, EPHCOM_MAXLINE, infp );
for ( j = 0; j < strlen( readbuf ); j++ )
if ( tolower( readbuf[j] ) == 'd' )
readbuf[j] = 'e';
datalines++;
//
// This is horrible, but use "%le" here and "%lE in the other
// ASCII data routine (ephcom_readascii_header) so gcc won't try
// to store the formats in the same location and write to them.
// (Problem with gcc not acting like K&R without -traditional flag
// and without -fwritable-strings flag.)
//
sscanf( readbuf, " %le %le %le", &val1, &val2, &val3 );
datablock[datapoints++] = val1;
if ( ( datapoints ) < header->ncoeff )
{
datablock[datapoints++] = val2;
if ( datapoints < header->ncoeff )
{
datablock[datapoints++] = val3;
}
}
}
}
return ( datapoints );
}
//! Read a JPL ephemeris binary header from the FILE pointed to by the
//! infp argument and store all header data in the ephcom_Header
//! struct pointed to by the header argument. If any errors are
//! detected this routine writes a message to stderr and exits.
//!
//! @param infp [IN ONLY]Pointer to a binary version of a JPL
//! ephemeris FILE.
//! @param header [OUT ONLY]Pointer to an ephcom_Header struct which
//! upon return will contain all the JPL ephemeris header information
//! that has been read from the FILE.
//!
void
ephcom_readbinary_header( FILE * infp, ephcom_Header *header )
{
int i, j, k;
if ( infp != stdin )
rewind( infp );
//
// Read title lines.
//
for ( i = 0; i < 3; i++ )
{
for ( j = 0; j < EPHCOM_MAXTTL; j++ )
{
header->ttl[i][j] = fgetc( infp );
}
if ( i == 0 && strncmp( header->ttl[0], "JPL ", 4 ) != 0 )
{
fprintf( stderr, "\nERROR: file is not a JPL ephemeris file.\n\n" );
if ( strncmp( header->ttl[0], "KSIZE", 5 ) == 0 )
fprintf( stderr, "File is an ASCII JPL ephemeris header instead.\n\n" );
exit( 1 );
}
header->ttl[i][j] = '\0';
}
//
// Read constant names.
//
for ( i = 0; i < 400; i++ )
{
for ( j = 0; j < 6; j++ )
{
header->cnam[i][j] = fgetc( infp );
}
header->cnam[i][j] = '\0';
}
//
// Read ephemeris start epoch, stop epoch, and step size (in Julian Days).
//
for ( i = 0; i < 3; i++ )
{
header->ss[i] = ephcom_indouble( infp );
}
// These values are half integral Julian dates. Make sure there is no
// numerical noise in these values.
header->ss[0] = ephcom_exact_time( header->ss[0] );
header->ss[1] = ephcom_exact_time( header->ss[1] );
// This value is an integral number of days (a power of two). Make sure there
// is no numerical noise in this value.
header->ss[2] = (double) (int) ( header->ss[2] + 0.01 );
//
// Read NCON, AU, EMRAT.
//
header->ncon = ephcom_inint( infp );
header->au = ephcom_indouble( infp );
header->emrat = ephcom_indouble( infp );
header->nval = header->ncon;
//
// Read indexes for coefficients in data block. Written in transposed
// order (Fortran and C matrices are transposed).
//
for ( i = 0; i < 12; i++ )
{
for ( j = 0; j < 3; j++ )
{
header->ipt[i][j] = ephcom_inint( infp );
}
}
header->numde = ephcom_inint( infp ); // Get ephemeris number
for ( i = 0; i < 3; i++ )
header->lpt[i] = ephcom_inint( infp );
//
// If there are no coefficients for an ipt[i][] object (i.e., ipt[i][1]==0),
// then ipt[i][0] should contain the value of the next available coefficient
// number rather than 0, as per communication of Myles Standish to Paul Hardy
// on preferred format of ephemeris headers.
//
// If there are no libration coefficients (i.e., lpt[1]==0), then lpt[0]
// should contain the value of the next available coefficient number rather
// than 0 as well, as per the same communication from Myles Standish.
//
// First set j to maximum index into ipt[] that has coefficients
j = 0;
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][1] > 0 && header->ipt[i][0] > j )
j = i;
// Now set j to next available index count.
if ( header->lpt[1] > 0 && header->lpt[0] > j )
j = header->lpt[1] + header->lpt[1] * header->lpt[2] * 3;
else
j = header->ipt[j][0] +
header->ipt[j][1] * header->ipt[j][2] * ( j == 11 ? 2 : 3 );
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][0] == 0 )
header->ipt[i][0] = j;
if ( header->lpt[0] == 0 )
header->lpt[0] = j;
//
// Set the maximum number of Chebyshev coefficients possible for this file,
// to initialize position and velocity Chebyshev coefficient arrays during
// Chebyshev interpolation.
//
header->maxcheby = 0;
for ( i = 0; i < 12; i++ )
if ( header->ipt[i][1] > header->maxcheby )
header->maxcheby = header->ipt[i][1];
if ( header->lpt[1] > header->maxcheby )
header->maxcheby = header->lpt[1];
//
// From JPL ephemeris number, set NCOEFF and calculate KSIZE = 2*NCOEFF.
//
// switch (header->numde) {
// case 102:
// header->ncoeff = 773;
// break;
// case 200:
// header->ncoeff = 826;
// break;
// case 202:
// header->ncoeff = 826;
// break;
// case 403:
// header->ncoeff = 1018;
// break;
// case 405:
// header->ncoeff = 1018;
// break;
// case 406:
// header->ncoeff = 728;
// break;
// case 410:
// header->ncoeff = 1018;
// break;
// default:
// header->ncoeff = 1018;
// break;
// }
//
// Calculate number of coefficients, starting with
// highest index into a data block (stored in j).
//
j = 0;
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][1] > 0 && header->ipt[i][0] > header->ipt[j][0] )
j = i;
//
// Now see if the starting point we found is lower than where
// lpt[] starts. If not, use lpt[] for largest value.
//
if ( header->lpt[1] > 0 && header->lpt[0] > header->ipt[j][0] )
{
header->ncoeff = header->lpt[0] - 1 + // starting point
( header->lpt[1] * // coefficients per coordinate
header->lpt[2] ) * // subblocks per block
3; // coordinates
}
else
{
header->ncoeff = header->ipt[j][0] - 1 + // starting point
( header->ipt[j][1] * // coefficients per coordinate
header->ipt[j][2] ) * // subblocks per block
( j == 11 ? 2 : 3 ); // coordinates
}
header->ksize = header->ncoeff + header->ncoeff; // KSIZE = 2*NCOEFF always
//
// Skip to second block in file.
//
fseek( infp, header->ncoeff * 8, SEEK_SET );
//
// Read ephemeris constants.
//
for ( i = 0; i < header->ncon; i++ )
{
header->cval[i] = ephcom_indouble( infp );
if ( strncmp( header->cnam[i], "NCOEFF", 6 ) == 0 )
{
header->ncoeff = header->cval[i];
header->ksize = 2 * header->cval[i];
}
else if ( strncmp( header->cnam[i], "LENUM ", 6 ) == 0 )
header->numle = header->cval[i];
}
if ( header->numle == 0 )
header->numle = header->numde;
}
//! Read a block of data coefficients from a JPL binary ephemeris file.
//!
//! @param infp [IN ONLY]Pointer to a binary version of a JPL
//! ephemeris FILE.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information that has already
//! been read from the infp FILE.
//! @param blocknum [IN ONLY]Requested direct access block number with
//! zero corresponding to the first data block after the two header
//! blocks in the binary ephemeris.
//! @param datablock [OUT ONLY]Pointer to an array that upon
//! successful return will be filled with datapoints == header->ncoeff
//! data points.
//! @returns number of coefficients read or 0 at EOF or some other i/o
//! error.
//!
int
ephcom_readbinary_block(
FILE *infp,
ephcom_Header *header,
int blocknum,
double *datablock
)
{
int i;
long filebyte;
filebyte = ( blocknum + 2 ) * header->ncoeff * 8; // 8 bytes per coefficient
fseek( infp, filebyte, SEEK_SET );
for ( i = 0; !feof( infp ) && !ferror( infp ) && i < header->ncoeff; i++ )
{
datablock[i] = ephcom_indouble( infp );
}
if ( feof( infp ) || ferror( infp ) )
i = 0; // 0 --> EOF or any other i/o error.
// First two values of data block are half-integral Julian dates. Make sure
// there is no numerical noise in these data. (This makes a difference for
// early versions of de422.)
if ( i >= 1 )
{
datablock[0] = ephcom_exact_time( datablock[0] );
datablock[1] = ephcom_exact_time( datablock[1] );
}
return ( i ); // Number of coefficients successfuly read (all or nothing).
}
//! Write JPL ephemeris header information in ASCII format.
//! @param outfp [IN ONLY]Pointer to the FILE which will be used to
//! output the formatted header information.
//! @param header [IN and OUT]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information to be output to the
//! FILE. However, some self-consistency adjustments of the header
//! are made before such FILE output and those are returned to the
//! calling routine as well.
//!
void
ephcom_writeascii_header( FILE * outfp, ephcom_Header *header )
{
char group[13];
double val1, val2, val3; // To read text line with 3 double precision words
int i, j, k, n;
int iword; // word number we're reading in a line
int blockout; // number of bytes we've written to current block/rec in file
int blockbytes; // number of bytes in a block, equals 8 * ncoeff
static char spaces[EPHCOM_MAXTTL] = " \n";
int idate[6];
const char *month[12] = { "JAN", "FEB", "MAR", "APR", "MAY", "JUN",
"JUL", "AUG", "SEP", "OCT", "NOV", "DEC" };
char writebuf[EPHCOM_MAXLINE + 1];
char outhcars[EPHCOM_MAXLINE + 1];
size_t fwrite( const void *ptr, size_t size, size_t nmemb, FILE *stream );
//
// First header line: KSIZE= # NCOEFF= #
//
blockbytes = 8 * header->ncoeff; // sizeof(double) * # of doubles/block
fprintf( outfp, "KSIZE=%5d NCOEFF=%5d\n", header->ksize, header->ncoeff );
if ( header->ksize != 2 * header->ncoeff )
{
fprintf( stderr, "Badly formed header; KSIZE <> 2*NCOEFF\n" );
exit( 1 );
}
//
// GROUP 1010: Title of ephemeris (DE/LE number, start JD, end JD)
//
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "GROUP 1010\n" );
fprintf( outfp, " \n" ); // blank line
//
// Header title lines with dates, for example:
//
// JPL Planetary Ephemeris DE405/LE405
// Start Epoch: JED= 2305424.5 1599 DEC 09 00:00:00
// Final Epoch: JED= 2525008.5 2201 FEB 20 00:00:00
//
sprintf( header->ttl[0], "JPL Planetary Ephemeris DE%03d/LE%03d",
header->numde, header->numle );
k = strlen( header->ttl[0] );
strcpy( &header->ttl[0][k], &spaces[k] );
ephcom_jd2cal( header->ss[0], idate, 0 );
sprintf( header->ttl[1], "Start Epoch: JED=%11.1f%5d %3s %02d %02d:%02d:%02d",
header->ss[0], idate[0], month[idate[1] - 1], idate[2],
idate[3], idate[4], idate[5] );
k = strlen( header->ttl[1] );
strcpy( &header->ttl[1][k], &spaces[k] );
ephcom_jd2cal( header->ss[1], idate, 0 );
sprintf( header->ttl[2], "Final Epoch: JED=%11.1f%5d %3s %02d %02d:%02d:%02d",
header->ss[1], idate[0], month[idate[1] - 1], idate[2],
idate[3], idate[4], idate[5] );
k = strlen( header->ttl[2] );
strcpy( &header->ttl[2][k], &spaces[k] );
//
// Don't print trailing blanks at the end of these 3 lines.
//
for ( i = 0; i < 3; i++ )
{
strncpy( writebuf, header->ttl[i], EPHCOM_MAXTTL + 1 );
for ( j = EPHCOM_MAXTTL; isspace( writebuf[j] ) || writebuf[j] == '\0'; j-- )
writebuf[j] = '\0';
// To match end space in JPL Epoch header lines.
if ( i > 0 )
writebuf[++j] = ' ';
fprintf( outfp, "%s\n", writebuf );
}
//
// GROUP 1030: Start and End JD, timestep (in JD) per block.
//
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "GROUP 1030\n" );
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "%12.2f%12.2f%11.0f.\n",
header->ss[0], header->ss[1], header->ss[2] );
//
// GROUP 1040: Constant names.
//
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "GROUP 1040\n" );
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "%6d\n", header->ncon );
//
// Now write the constant names, 10 per line, each 6 characters long
// preceded by 2 blanks. Pad names with blanks to make 6 characters.
//
for ( i = 0; i < header->ncon; i++ )
{
fprintf( outfp, " %-6s", header->cnam[i] );
if ( i % 10 == 9 )
fprintf( outfp, "\n" );
}
if ( i % 10 != 0 ) // Pad last line with spaces (i is 1 more than above)
{
for (; i % 10 != 0; i++ )
fprintf( outfp, " " );
fprintf( outfp, "\n" );
}
//
// GROUP 1041: Constant values.
//
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "GROUP 1041\n" );
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "%6d\n", header->nval );
if ( header->nval != header->ncon )
{
fprintf( stderr, "Error: number of constants and values not equal.\n\n" );
exit( 1 );
}
//
// Now write constant values, 3 per line, 26 characters each.
//
for ( i = 0; i < header->ncon; i += 3 )
{
val1 = header->cval[i];
val2 = ( i + 1 < header->ncon ) ? header->cval[i + 1] : 0.0;
val3 = ( i + 2 < header->ncon ) ? header->cval[i + 2] : 0.0;
// Write values, 3 coefficients per line, pad lines with 0.0E+00
// Must have trailing blank to make room for reformatted
// fortran version (with leading "0.") created below.
// Note there is (just) room for Windows 3-digit exponent in
// the format.
sprintf( writebuf, "%25.17E %25.17E %25.17E ", val1, val2, val3 );
// Now re-format numbers the way the JPL header file writes them:
// all with a leading "0.", so the exponent is one greater.
// If the number is written in Windows 3-digit exponent format,
// then it is shifted by one byte to the right to overwrite
// the assumed leading 0 of the exponent (or error out if
// there are three exponent digits but the leading one is not
// zero, i.e., this logic will not work for numbers greater
// than or equal to 1.e100 or less than or equal to 1.e-101, but
// this limitation is also in the current JPL ascii format which
// we are trying to mimic as closely as possible here.
ephcom_doublestrc2f( &writebuf[0] ); // Reformat first number
ephcom_doublestrc2f( &writebuf[26] ); // Reformat second number
ephcom_doublestrc2f( &writebuf[52] ); // Reformat third number
fprintf( outfp, "%s\n", writebuf );
}
//
// GROUP 1050: Constant values.
//
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "GROUP 1050\n" );
fprintf( outfp, " \n" ); // blank line
//
// If there are no coefficients for an ipt[i][] object (i.e., ipt[i][1]==0),
// then ipt[i][0] should contain the value of the next available coefficient
// number rather than 0, as per communication of Myles Standish to Paul Hardy
// on preferred format of ephemeris headers.
//
// If there are no libration coefficients (i.e., lpt[1]==0), then lpt[0]
// should contain the value of the next available coefficient number rather
// than 0 as well, as per the same communication from Myles Standish.
//
// First set j to maximum index into ipt[] that has coefficients
j = 0;
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][1] > 0 && header->ipt[i][0] > j )
j = i;
// Now set j to next available index count.
if ( header->lpt[1] > 0 && header->lpt[0] > j )
j = header->lpt[1] + header->lpt[1] * header->lpt[2] * 3;
else
j = header->ipt[j][0] +
header->ipt[j][1] * header->ipt[j][2] * ( j == 11 ? 2 : 3 );
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][0] == 0 )
header->ipt[i][0] = j;
if ( header->lpt[0] == 0 )
header->lpt[0] = j;
//
// Write ipt array in transposed order (arrays are transposed in FORTRAN
// from their order in C).
//
for ( i = 0; i < 3; i++ )
{
for ( j = 0; j < 12; j++ )
{
fprintf( outfp, "%6d", header->ipt[j][i] );
}
fprintf( outfp, "%6d\n", header->lpt[i] );
}
//
// GROUP 1070: Constant values.
//
fprintf( outfp, " \n" ); // blank line
fprintf( outfp, "GROUP 1070\n" );
fprintf( outfp, " \n" ); // blank line
//
// Now we're pointing to the first block of coefficient data, after header.
//
}
//! Write JPL ephemeris coefficient block of data in ASCII format.
//! @param outfp [IN ONLY]Pointer to the FILE which will be used to
//! output the formatted block of data.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information. Some of these
//! data are included in the formatted block and some of these
//! data are used to control how much is written in that formatted block.
//! @param blocknum [IN ONLY]Block number. This value + 1 will be used
//! in the output formatted block of data.
//! @param datablock [IN ONLY]Pointer to an array that contains the
//! block of data that will be output in formatted form.
//!
void
ephcom_writeascii_block(
FILE * outfp,
ephcom_Header *header,
int blocknum,
double *datablock )
{
double val1, val2, val3; // To write text line with 3 double precision words
int i, j, k, n;
char writebuf[EPHCOM_MAXLINE + 1];
char outhcars[EPHCOM_MAXLINE + 1];
size_t fwrite( const void *ptr, size_t size, size_t nmemb, FILE *stream );
int fputc( int, FILE * );
//
// Write first line in block, which is block number and ncoeff.
//
fprintf( outfp, "%6d%6d\n", blocknum + 1, header->ncoeff );
//
// Now write the data, 3 coefficients per line, 26 characters each.
// Convert format to match what appears in JPL Ephemeris ASCII files.
//
for ( i = 0; i < header->ncoeff; i += 3 )
{
val1 = datablock[i];
val2 = ( i + 1 ) < header->ncoeff ? datablock[i + 1] : 0.0;
val3 = ( i + 2 ) < header->ncoeff ? datablock[i + 2] : 0.0;
// Write values, 3 coefficients per line, pad lines with 0.0E+00
// Must have trailing blank to make room for reformatted
// fortran version (with leading "0.") created below.
// Note there is (just) room for Windows 3-digit exponent in
// the format.
sprintf( writebuf, "%25.17E %25.17E %25.17E ", val1, val2, val3 );
// Now re-format numbers the way the JPL header file writes them:
// all with a leading "0.", so the exponent is one greater.
// If the number is written in Windows 3-digit exponent format,
// then it is shifted by one byte to the right to overwrite
// the assumed leading 0 of the exponent (or error out if
// there are three exponent digits but the leading one is not
// zero, i.e., this logic will not work for numbers greater
// than or equal to 1.e100 or less than or equal to 1.e-101, but
// this limitation is also in the current JPL ascii format which
// we are trying to mimic as closely as possible here.
ephcom_doublestrc2f( &writebuf[0] ); // Reformat first number
ephcom_doublestrc2f( &writebuf[26] ); // Reformat second number
ephcom_doublestrc2f( &writebuf[52] ); // Reformat third number
fprintf( outfp, "%s\n", writebuf );
}
}
//! Write JPL ephemeris header information in binary form.
//! @param outfp [IN ONLY]Pointer to the FILE which will be used to
//! output the binary header information.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information to be output in
//! binary form.
//!
void
ephcom_writebinary_header( FILE *outfp, ephcom_Header *header )
{
char readbuf[EPHCOM_MAXLINE + 1];
char group[13]; // To hold "GROUP" header line
int blockout; // number of bytes we've written to current block/rec in file
int blockbytes; // number of bytes in a block, equals 8 * ncoeff
double val1, val2, val3; // To read text line with 3 double precision words
int i, j, k, n;
int idate[6];
const char *month[12] = { "JAN", "FEB", "MAR", "APR", "MAY", "JUN",
"JUL", "AUG", "SEP", "OCT", "NOV", "DEC" };
char outhcars[EPHCOM_MAXLINE + 1];
size_t fwrite( const void *ptr, size_t size, size_t nmemb, FILE *stream );
//
// Point to beginning of output file.
//
rewind( outfp );
//
// First header line: KSIZE= # NCOEFF= #
//
blockbytes = sizeof ( double ) * header->ncoeff;
//
// Start writing output ephemeris, beginning with header.
//
//
// Header title lines with dates, for example:
//
// JPL Planetary Ephemeris DE405/LE405
// Start Epoch: JED= 2305424.5 1599 DEC 09 00:00:00
// Final Epoch: JED= 2525008.5 2201 FEB 20 00:00:00
//
sprintf( header->ttl[0], "JPL Planetary Ephemeris DE%03d/LE%03d",
header->numde, header->numle );
for ( i = strlen( header->ttl[0] ); i < EPHCOM_MAXTTL; i++ )
header->ttl[1][i] = ' ';
ephcom_jd2cal( header->ss[0], idate, 0 );
sprintf( header->ttl[1], "Start Epoch: JED=%11.1f%5d %3s %02d %02d:%02d:%02d",
header->ss[0], idate[0], month[idate[1] - 1], idate[2],
idate[3], idate[4], idate[5] );
for ( i = strlen( header->ttl[1] ); i < EPHCOM_MAXTTL; i++ )
header->ttl[1][i] = ' ';
ephcom_jd2cal( header->ss[1], idate, 0 );
sprintf( header->ttl[2], "Final Epoch: JED=%11.1f%5d %3s %02d %02d:%02d:%02d",
header->ss[1], idate[0], month[idate[1] - 1], idate[2],
idate[3], idate[4], idate[5] );
for ( i = strlen( header->ttl[2] ); i < EPHCOM_MAXTTL; i++ )
header->ttl[2][i] = ' ';
header->ttl[0][EPHCOM_MAXTTL] = header->ttl[1][EPHCOM_MAXTTL] = header->ttl[2][EPHCOM_MAXTTL] = '\0';
//
// ephcom_Header title lines.
//
// Write the three title lines to the output file, padded with blanks,
// 84 characters long (84 is the first even multiple of 6 that is > 80,
// so the JPL software uses that value because it reads in Fortran 'A6'
// character strings.
//
fprintf( outfp, "%-84s%-84s%-84s", header->ttl[0], header->ttl[1], header->ttl[2] );
blockout = 3 * EPHCOM_MAXTTL; // Just wrote 3 84-byte strings to start output file
//
// Now output 400 cnam entries to the output file.
//
for ( i = 0; i < header->ncon; i++ )
{
fprintf( outfp, "%-6s", header->cnam[i] );
blockout += 6;
}
for (; i < 400; i++ )
{
fprintf( outfp, " " ); // Round out to 400 entries, all blank at end
blockout += 6;
}
//
// Binary values: Make sure bytes are in big-endian (network) order for file.
//
for ( i = 0; i < 3; i++ )
{
ephcom_outdouble( outfp, header->ss[i] ); // Write net-order bytes from double precision
blockout += 8;
}
ephcom_outint( outfp, header->ncon );
blockout += 4;
ephcom_outdouble( outfp, header->au );
blockout += 8;
ephcom_outdouble( outfp, header->emrat );
blockout += 8;
//
// If there are no coefficients for an ipt[i][] object (i.e., ipt[i][1]==0),
// then ipt[i][0] should contain the value of the next available coefficient
// number rather than 0, as per communication of Myles Standish to Paul Hardy
// on preferred format of ephemeris headers.
//
// If there are no libration coefficients (i.e., lpt[1]==0), then lpt[0]
// should contain the value of the next available coefficient number rather
// than 0 as well, as per the same communication from Myles Standish.
//
// First set j to maximum index into ipt[] that has coefficients
j = 0;
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][1] > 0 && header->ipt[i][0] > j )
j = i;
// Now set j to next available index count.
if ( header->lpt[1] > 0 && header->lpt[0] > j )
j = header->lpt[1] + header->lpt[1] * header->lpt[2] * 3;
else
j = header->ipt[j][0] +
header->ipt[j][1] * header->ipt[j][2] * ( j == 11 ? 2 : 3 );
for ( i = 1; i < 12; i++ )
if ( header->ipt[i][0] == 0 )
header->ipt[i][0] = j;
if ( header->lpt[0] == 0 )
header->lpt[0] = j;
for ( j = 0; j < 12; j++ )
{
for ( i = 0; i < 3; i++ )
{
ephcom_outint( outfp, header->ipt[j][i] );
blockout += 4;
}
}
ephcom_outint( outfp, header->numde );
blockout += 4;
for ( i = 0; i < 3; i++ )
{
ephcom_outint( outfp, header->lpt[i] );
blockout += 4;
}
//
// Now pad the end of the first record with null bytes. Note: the
// JPL Fortran software just skips to next record at this point.
//
for ( i = blockout; i < blockbytes; i++ )
{
fputc( '\0', outfp );
}
//
// End of first block. Now set blockout to 0 and start with next block.
//
blockout = 0;
for ( i = 0; i < header->ncon; i++ )
{
ephcom_outdouble( outfp, header->cval[i] );
blockout += 8;
}
//
// Pad with double-precision zeroes for rest of array.
//
for (; i < 400; i++ )
{
ephcom_outdouble( outfp, (double) 0.0 );
blockout += 8;
}
//
// Pad with nulls for rest of block.
//
for ( i = blockout; i < blockbytes; i++ )
{
fputc( '\0', outfp );
}
//
// Finished normally.
//
}
//! Write JPL ephemeris coefficient block of data in binary form.
//! @param outfp [IN ONLY]Pointer to the FILE which will be used to
//! output the binary block of data.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information. Some of these
//! data are used to control where in the binary FILE the block of
//! data is written and how large it is.
//! @param blocknum [IN ONLY]Block number. This value helps control
//! where in the binary FILE the block of data is written.
//! @param datablock [IN ONLY]Pointer to an array that contains the
//! block of data that will be output in binary form.
//!
void
ephcom_writebinary_block(
FILE * outfp,
ephcom_Header *header,
int blocknum,
double *datablock )
{
int i;
int filebyte;
int filepos;
//
// Find out where we need to point in the binary file.
//
filebyte = ( blocknum + 2 ) * header->ncoeff * 8; // 8 bytes per coefficient
//
// If the file isn't that large, pad it with null bytes
//
fseek( outfp, 0L, SEEK_END );
filepos = ftell( outfp );
if ( filepos < filebyte )
{
for ( i = 0; i < ( filebyte - filepos ); i++ )
{
fputc( '\0', outfp );
}
}
//
// Now go to position where we want to start writing.
//
fseek( outfp, filebyte, SEEK_SET );
for ( i = 0; i < header->ncoeff; i++ )
{
ephcom_outdouble( outfp, datablock[i] );
}
}
//! Write out a block of JPL binary data in ascii form that is nicely
//! formatted and therefore verbose.
//!
//! @param outfp [IN ONLY]Pointer to the FILE which will be used to
//! output the nicely formatted data.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information. Some of these
//! data are used to control how to output the block of data in a
//! nicely formatted way.
//! @param datablock [IN ONLY]Pointer to an array that contains the
//! block of data that will be output in nicely formatted form.
//!
void
ephcom_parse_block(
FILE * outfp,
ephcom_Header *header,
double *datablock )
{
int i0, i1, i2, i3;
int blockword;
//
// Names of the objects in Chebyshev coefficient arrays.
//
const char *ephcom_coeffname[13] = {
"Mercury", "Venus", "EMBary", "Mars", "Jupiter", "Saturn", "Uranus", "Neptune",
"Pluto", "Geocentric Moon", "Sun", "Nutation", "Libration"
};
blockword = 0;
fprintf( outfp, "@%04d StartJD\t%12.2f\n", blockword++, datablock[0] );
fprintf( outfp, "@%04d EndJD\t%12.2f\n", blockword++, datablock[1] );
for ( i0 = 0; i0 < 13; i0++ ) // For all bodies
{
fprintf( outfp, "Body\t%d (%s)\n", i0 + 1, ephcom_coeffname[i0] );
for ( i1 = 0; i1 < header->ipt[i0][2]; i1++ ) // For all subintervals
{
fprintf( outfp, " Subinterval %d of %d\n", i1 + 1, header->ipt[i0][2] );
for ( i2 = 0; i2 < ( i0 == 11 ? 2 : 3 ); i2++ ) // For all coordinates
{
fprintf( outfp, " %cCoefficients\n", 'X' + i2 );
for ( i3 = 0; i3 < header->ipt[i0][1]; i3++ ) // For all coefficients
{
blockword = header->ipt[i0][0] +
i1 * header->ipt[i0][1] * ( i0 == 11 ? 2 : 3 ) +
i2 * header->ipt[i0][1] + i3 - 1;
fprintf( outfp, " @%04d [%2d of %2d] %25.17E\n",
blockword, i3 + 1, header->ipt[i0][1], datablock[blockword] );
}
}
}
}
}
//! Read the next two lines of the ascii form of a JPL ephemeris file.
//! For the last of those check that it is exactly the same as the
//! expected group header form, that is, 12 characters containing
//! "GROUP nnnn" with the same nnnn as expected. If the group is not
//! what is expected, then print an error message and exit.
//!
//! @param group [OUT ONLY]Pointer to a group header that upon return
//! will be filled by a 12-character null-terminated string that we
//! read.
//! @param expected [IN ONLY]Pointer to a 12-character null-terminated
//! string that we expect to read.
//! @param infile [IN ONLY]Pointer to the JPL ascii ephemeris FILE
//! that we read.
//!
static void
ephcom_nxtgrp( char *group, const char *expected, FILE *infile )
{
char readbuf[EPHCOM_MAXLINE + 1];
fgets( readbuf, EPHCOM_MAXLINE, infile ); // Blank Line
fgets( readbuf, EPHCOM_MAXLINE, infile ); // "GROUP dddd\n"
strncpy( group, readbuf, 12 );
group[12] = '\0';
if ( strncmp( group, expected, 12 ) != 0 )
{
fprintf( stderr, "Badly formed header; \"%s\" not found.\n\n", expected );
exit( 1 );
}
fgets( readbuf, EPHCOM_MAXLINE, infile ); // Blank Line
}
//! Write a double-precision value to the given binary file with
//! bytes swapped if necessary to match network order (Big Endian).
//! On Intel 80x86 the bytes will get swapped, on Motorola or SPARC
//! they won't.
//!
//! @param outfp [IN ONLY]Pointer to the binary output FILE.
//! @param x [IN ONLY]Double-precision value that will be written to
//! the binary FILE.
//!
static void
ephcom_outdouble( FILE *outfp, double x )
{
double retval;
unsigned char ch[8];
memcpy( (void *) ch, (const void *) &x, 8 );
gnulliver64c( ch );
fwrite( ch, 1, 8, outfp );
}
//! Write a integer value to the given binary file with bytes swapped
//! if necessary to match network order (Big Endian). On Intel 80x86
//! the bytes will get swapped, on Motorola or SPARC they won't.
//!
//! @param outfp [IN ONLY]Pointer to the binary output FILE.
//! @param u [IN ONLY]Integer value that will be written to the binary
//! FILE.
//!
static void
ephcom_outint( FILE * outfp, unsigned u )
{
unsigned u2;
u2 = gnulliver32( u );
fwrite( &u2, 4, 1, outfp );
}
//! Read a double-precision value from the given binary file with
//! bytes swapped if necessary to match host endian order. On Intel
//! 80x86 the bytes will get swapped, on Motorola or SPARC they won't.
//!
//! @param infp [IN ONLY]Pointer to the binary input FILE.
//! @returns the (possibly) byte-swapped double-precision value that
//! was read from the binary input FILE.
//!
double
ephcom_indouble( FILE *infp )
{
double x;
double retval;
unsigned char ch[8];
//
// Handle as character string until bytes are in correct order,
// then copy to double once they are.
//
fread( ch, 1, 8, infp );
gnulliver64c( ch );
memcpy( (void *) &retval, (const void *) ch, (size_t) 8 );
return ( retval );
}
//! Read an integer value from the given binary file with bytes
//! swapped if necessary to match host endian order. On Intel 80x86
//! the bytes will get swapped, on Motorola or SPARC they won't.
//!
//! @param infp [IN ONLY]Pointer to the binary input FILE.
//! @returns the (possibly) byte-swapped integer value that was read
//! from the binary input FILE.
//!
int
ephcom_inint( FILE *infp )
{
unsigned u;
int retval;
fread( &u, 4, 1, infp );
retval = (int) gnulliver32( u );
return ( retval );
}
//! Function to convert a string with a double precision value written
//! in C to a double precision value that fortran understands (i.e.,
//! with a "D" exponent character). Conversion happens in place.
//!
//! @param buf [IN AND OUT]Pointer to a character string holding the C
//! double-precision value (in "E" exponential format with a trailing
//! blank after the exponent to make room for the leading zero
//! notation of the fortran value) on input and the fortran
//! double-precision value in "D" exponential format for fortran (with
//! leading zero before the decimal point) on output. If the resulting
//! fortran exponent has a leading zero and more than two digits that
//! leading zero is dropped while right justification is maintained
//! by shifting the whole string to the right by one byte to overlay
//! that leading zero by the exponent sign.
//!
static void
ephcom_doublestrc2f( char *buf )
{
int i, j, istart, istop, exp, edigits;
double x;
// Deal with three or more digit exponent with leading zero
// (which can occur for the Windows case).
for ( istop = 0; toupper( buf[istop] ) != 'E'; istop++ )
;
// buf[istop] is 'E', buf[istop+1] is the exponent sign, buf[istop+2],...
// is the absolute value of the exponent.
if ( buf[istop + 2] == '0' && isdigit( buf[istop + 3] ) && isdigit( buf[istop + 4] ) )
{
for ( istart = istop + 2; istart > 0; istart-- )
buf[istart] = buf[istart - 1];
buf[0] = ' ';
istop++;
}
for ( istart = 0; isspace( buf[istart] ); istart++ )
;
x = atof( &buf[istart] );
exp = atoi( &buf[istop + 1] );
exp++;
if ( exp < 0 )
{
buf[istop + 2] = '-';
exp = -exp;
}
else
{
buf[istop + 2] = '+';
}
if ( x == 0.0 )
exp = 0;
if ( exp < 100 )
edigits = 2;
else if ( exp < 1000 )
edigits = 3;
else
edigits = 4;
while ( edigits > 0 )
{
buf[istop + edigits + 2] = exp % 10 + '0';
exp /= 10;
edigits--;
}
buf[istop + 1] = 'D';
while ( istop > istart && buf[istop - 1] != '.' )
{
buf[istop] = buf[istop - 1];
istop--;
}
buf[istop] = buf[istop - 2]; // buf[istop-1] == '.'
buf[istop - 2] = '0'; // leading zero
}
//! This ephcom_pleph routine takes coordinates already calculated in
//! a ephcom_Coords struct and returns selected results in an array
//! depending on the ntarg and ncentr indices provided by the calling
//! routine. These indices have the following interpretation (note
//! the offset of one compared to the interpretation of the first index
//! of pv in the ephcom_Coords struct.
//! <table border>
//! <tr> <td><b>Index</b></td> <td><b>Identification</b></td> </tr>
//! <tr> <td>1</td> <td>Mercury</td> </tr>
//! <tr> <td>2</td> <td>Venus</td> </tr>
//! <tr> <td>3</td> <td>Earth</td> </tr>
//! <tr> <td>4</td> <td>Mars</td> </tr>
//! <tr> <td>5</td> <td>Jupiter</td> </tr>
//! <tr> <td>6</td> <td>Saturn</td> </tr>
//! <tr> <td>7</td> <td>Uranus</td> </tr>
//! <tr> <td>8</td> <td>Neptune</td> </tr>
//! <tr> <td>9</td> <td>Pluto</td> </tr>
//! <tr> <td>10</td> <td>Moon</td> </tr>
//! <tr> <td>11</td> <td>Sun</td> </tr>
//! <tr> <td>12</td> <td>Solar System Barycenter</td> </tr>
//! <tr> <td>13</td> <td>Earth-Moon Barycenter</td> </tr>
//! <tr> <td>14</td> <td>Nutation Angles</td> </tr>
//! <tr> <td>15</td> <td>Libration Angles</td> </tr>
//! <tr> <td>16</td> <td>Moon (Geocentric)</td> </tr>
//! </table>
//!
//! @param coords [IN ONLY]Pointer to a ephcom_Coords struct which
//! contains interpolated values of all coordinates and their time derivatives
//! as calculated from Chebyshev coefficients supplied by a JPL ephemeris.
//! @param ntarg [IN ONLY]Index interpreted according to the
//! above table which identifies the "target" data in coords.
//! @param ncntr [IN ONLY]Index interpreted according to the above
//! table which identifies the "center" data in coords. If either
//! ntarg or ncent is 14, the interpolated nutation angle data (two
//! angles and two angle time derivatives) are returned in r.
//! Otherwise, if either ntarg or ncent is 15, the interpolated
//! libration angle data (three angles and three angle time
//! derivatives) are returned in r. Otherwise, if either ntarg or
//! ncent is 16, the moon geocentric position and velocity data (3
//! positions and 3 velocities) are returned in pv. Otherwise (the
//! normal case) if 0 < ntarg < 14 and 0 < ncent < 14, the
//! interpolated positions and velocities corresponding to the center
//! index are subtracted from the interpolated positions and
//! velocities corresponding to the target index and the resulting
//! data (3 positions and 3 velocities) are returned in pv.
//! Otherwise, ephcom_pleph() issues an error message and exits.
//! @param r [OUT ONLY]Pointer to an array which upon return will be
//! filled with the requested interpolated results (4 values for
//! nutation and 6 values for everything else).
//!
void
ephcom_pleph( ephcom_Coords *coords, int ntarg, int ncntr, double *r )
{
int i;
if ( ntarg == 14 || ncntr == 14 )
{
for ( i = 0; i < 4; i++ )
r[i] = coords->pv[13][i];
}
else if ( ntarg == 15 || ncntr == 15 )
{
for ( i = 0; i < 6; i++ )
r[i] = coords->pv[14][i];
}
else if ( ntarg == 16 || ncntr == 16 )
{
for ( i = 0; i < 6; i++ )
r[i] = coords->pv[15][i];
}
else if ( ( 0 < ntarg && ntarg < 14 ) && ( 0 < ncntr && ncntr < 14 ) )
{
for ( i = 0; i < 6; i++ )
r[i] = coords->pv[ntarg - 1][i] - coords->pv[ncntr - 1][i];
}
else
{
fprintf( stderr, "ephcom_pleph: Invalid combination of ntarg = %d and ncntr = %d\n", ntarg, ncntr );
exit( EXIT_FAILURE );
}
}
//! Interpolate positions and velocities of all stored JPL "bodies" at given time from a JPL
//! binary ephemeris file. Transform the interpolated data to the following index scheme
//! for JPL bodies where the index is one less than the index used for the arguments
//! of ephcom_pleph():
//! <table border>
//! <tr> <td><b>Index</b></td> <td><b>Identification</b></td> </tr>
//! <tr> <td>0</td> <td>Mercury</td> </tr>
//! <tr> <td>1</td> <td>Venus</td> </tr>
//! <tr> <td>2</td> <td>Earth</td> </tr>
//! <tr> <td>3</td> <td>Mars</td> </tr>
//! <tr> <td>4</td> <td>Jupiter</td> </tr>
//! <tr> <td>5</td> <td>Saturn</td> </tr>
//! <tr> <td>6</td> <td>Uranus</td> </tr>
//! <tr> <td>7</td> <td>Neptune</td> </tr>
//! <tr> <td>8</td> <td>Pluto</td> </tr>
//! <tr> <td>9</td> <td>Moon</td> </tr>
//! <tr> <td>10</td> <td>Sun</td> </tr>
//! <tr> <td>11</td> <td>Solar System Barycenter</td> </tr>
//! <tr> <td>12</td> <td>Earth-Moon Barycenter</td> </tr>
//! <tr> <td>13</td> <td>Nutation Angles</td> </tr>
//! <tr> <td>14</td> <td>Libration Angles</td> </tr>
//! <tr> <td>15</td> <td>Moon (Geocentric)</td> </tr>
//! </table>
//!
//! @param infp [IN ONLY]Pointer to a binary version of a JPL
//! ephemeris FILE.
//! @param header [IN ONLY]Pointer to an ephcom_Header struct which
//! contains the JPL ephemeris header information that has already
//! been read from that binary JPL ephemeris FILE.
//! @param coords [IN AND OUT]Pointer to a ephcom_Coords struct which
//! contains on input coords->et2 (the split Julian date where the
//! interpolation should occur) and also the control information
//! coords->km (if nonzero, solar system body coordinates [but not
//! nutation and libration angles which are always returned in
//! radians] will be be returned in kilometers rather than
//! astronomical units); coords->second (if nonzero, all solar system
//! body and nutation and libration angle time derivatives will be
//! returned in per second units rather than in per day units);
//! coords->bary (if nonzero, all solar system body coordinates will
//! be relative to the solar system barycenter, otherwise they will be
//! relative to the solar system body indicated by the coords->center
//! index; and coords->center (the index in the range from 0 to 12
//! which cooresponds to a particular solar system body indicated in
//! the above table, and which only needs to be supplied if
//! coords->bary is zero). Upon return this struct contains
//! interpolated values of all coordinates and their time derivatives
//! as calculated from the Chebyshev coefficients in datablock using
//! the above body index scheme.
//! @param datablock [OUT ONLY]Pointer to an array that upon return
//! will contain the block of Chebyshev coefficient data that has been
//! read that has a Julian date range that contains the specified
//! Julian date in coords where the interpolation occurred.
//! @returns 0 on success and -1 on failure (due to specified Julian
//! date in coords out of range or some i/o error).
//!
int
ephcom_get_coords( FILE * infp,
ephcom_Header *header,
ephcom_Coords *coords,
double *datablock )
{
double et2[2], pjd[2]; // Ephemeris times, split into coarse (whole) and fine time in JD
double filetime; // JDs since start of ephemeris file
double blocktime[2]; // JDs since start of data block
double subtime; // JDs since start of subinterval in block
int i, j, k;
int blocknum;
// Number of subintervals in data block for this body
int nsub;
// Number of subinterval for this body
int subinterval;
// Offset in datablock for current body and subinterval
int dataoffset;
// Span of one subinterval in days
double subspan;
// Span of one subinterval in days (coords->second is zero) or
// seconds (coords->second is nonzero) used for normalization
// of the Chebyshev polynomial time derivatives.
double norm_span;
// Normalized Chebyshev time, in interval [-1,1].
double chebytime;
// Number of coordinates for position and velocity
int ncoords;
// Number of Chebyshev coefficients per coordinate
int ncf;
// Return value
int retval;
// Assume normal return
retval = 0;
// et2 is a transformed version of coords->et2 such that the first
// value of et2 is exactly half-integral to match the exactly
// half-integral characteristics of the Julian dates returned from
// the binary ephemeris.
et2[1] = ephcom_split( coords->et2[0] - 0.5, &et2[0] );
pjd[1] = ephcom_split( coords->et2[1], &pjd[0] );
// et2[0] should end up as exactly half integral.
et2[0] += pjd[0] + 0.5;
// Deal with fractional remainders.
et2[1] = ephcom_split( et2[1] + pjd[1], &pjd[0] );
et2[0] += pjd[0];
if ( et2[0] + et2[1] < header->ss[0] || et2[0] + et2[1] > header->ss[1] )
{
// fprintf(stderr,"Time is outside ephemeris range.\n");
retval = -1;
}
else
{
// Days from start of file. First part of this calculation should be
// exact because both values are exactly half integral.
filetime = ( et2[0] - header->ss[0] ) + et2[1];
// Data block in file (offset by two in ephcom_readbinary_block to skip two
// header blocks).
// blocknum is initially calculated using the convention that the time is
// in the semi-open interval [datablock[0], datablock[1]), i.e., is
// strictly less than datablock[1].
blocknum = (int) ( filetime / header->ss[2] );
// If time corresponds to datablock[1] of the last block =
// header->ss[1], then change the above convention to allow
// time to correspond to that value, that is calculate
// blocknum index as if the time was just slightly less than
// header->ss[1].
if ( et2[0] == header->ss[1] && et2[1] == 0 )
blocknum--;
// Read the data block that contains the coefficients for the
// desired date.
if ( ephcom_readbinary_block( infp, header, blocknum, datablock ) <= 0 )
{
retval = -1;
}
else
{
// Now step through the bodies and interpolate positions
// and velocities.
// Days from block start. blocktime[0] calculation should
// be exact because both values exactly half integral.
blocktime[0] = et2[0] - datablock[0];
blocktime[1] = et2[1];
for ( i = 0; i < 13; i++ )
{
// The i index corresponds to positions and velocities
// of solar system bodies, two nutation angles and
// their time derivatives, or 3 lunar libration angles
// and their time derivatives as noted in the
// following table. (The positions and velocities are
// solar system barycentric unless noted otherwise.)
// 0 = Mercury
// 1 = Venus
// 2 = Earth-Moon barycenter
// 3 = Mars
// 4 = Jupiter
// 5 = Saturn
// 6 = Uranus
// 7 = Neptune
// 8 = Pluto
// 9 = Moon (Geocentric)
// 10 = Sun
// 11 = nutation angles
// 12 = lunar librations
// subspan is always an integer; header->ss[2] is
// either 2^5 or 2^6 while header->ipt[i][2] is always
// a low (< 5) power of two.
subspan = header->ss[2] / header->ipt[i][2]; // Days/subinterval
norm_span = coords->seconds ? subspan * 86400.0 : subspan;
subinterval = (int) ( ( ( et2[0] - datablock[0] ) + et2[1] ) / subspan );
// For this corner case calculate the subinterval value as
// if the time were slightly less than header->ss[1] (which
// is equal to datablock[1] in this special case).
if ( et2[0] == header->ss[1] && et2[1] == 0 )
subinterval--;
ncoords = i == 11 ? 2 : 3; // 2 coords for nutation, else 3
dataoffset = header->ipt[i][0] - 1 +
ncoords * header->ipt[i][1] * subinterval;
// header->ss[2] / header->ipt[i][2] is always an
// integer; header->ss[2] is either 2^5 or 2^6 while
// header->ipt[i][2] is always a low (< 5) power of
// two.
subtime = ( blocktime[0] - subinterval * header->ss[2] / header->ipt[i][2] ) + blocktime[1];
//
// Divide days in this subblock by total days in
// subblock to get interval [0,1]. The right part of
// the expression will evaluate to a whole number:
// subinterval lengths are all integer multiples of
// days in a block (all powers of 2).
//
chebytime = subtime / subspan;
chebytime = ( chebytime + chebytime ) - 1.0;
if ( chebytime < -1.0 || chebytime > 1.0 )
{
fprintf( stderr, "Chebyshev time is beyond [-1,1] interval.\n" );
fprintf( stderr,
"filetime=%f, blocktime[0]=%f, blocktime[1]=%f, subtime=%f, chebytime=%f\n",
filetime, blocktime[0], blocktime[1], subtime, chebytime );
}
else
{
//
// Everything is as expected. Interpolate
// coefficients to calculate position and velocity
// (or angles and angles' time derivatives for the
// case of nutation or libration) for the ith
// "body" in the solar system at time equivalent
// to chebytime. The number of coordinates is
// ncoords which is 3 for everything but nutation
// where it is 2.
//
ephcom_cheby( header->maxcheby, chebytime, norm_span,
&datablock[dataoffset],
ncoords, header->ipt[i][1], coords->pv[i] );
}
}
//
// Set any user-defined coordinates to zero.
//
// for (i = 16; i < EPHCOM_NUMOBJECTS; i++)
// coords->pv[i][0] = coords->pv[i][1] = coords->pv[i][1] =
// coords->pv[i][1] = coords->pv[i][1] = coords->pv[i][1] = 0.0;
//
// With interpolations complete, calculate Earth from EMBary and
// Sun from SSBary. Preserve other coordinates.
// N.B. last two elements of nutation are undefined, but
// as a result of this next loop those locations are zeroed
// so that all 6 components of each coords->pv[] vector
// are initialized.
for ( j = 0; j < 6; j++ )
{
// Save original lunar geocentric coords
coords->pv[15][j] = coords->pv[ 9][j];
// Save Librations if on file
coords->pv[14][j] = coords->pv[12][j];
// Save Nutations if on file. Last two components
// are uninitialized so avoid them.
if ( j < 4 )
{
coords->pv[13][j] = coords->pv[11][j];
}
// Save Earth-Moon barycenter.
coords->pv[12][j] = coords->pv[2][j];
// Prepare new solar system barycenter coordinates (relative
// to that center). Note, this action initializes the
// last two components of pv[11] (previously used
// for nutation) for the first time.
coords->pv[11][j] = 0.;
//
// Calculate Earth and Moon from EMBary and geocentric Moon.
//
// New Earth
coords->pv[2][j] -= coords->pv[9][j] / ( 1.0 + header->emrat );
// New Moon
coords->pv[9][j] += coords->pv[2][j];
// The first index corresponds to positions and velocities
// of solar system bodies, two nutation angles and
// their time derivatives, or 3 lunar libration angles
// and their time derivatives as noted in the
// following table. (The positions and velocities are
// solar system barycentric unless noted otherwise. An
// asterisk preceding a number indicates a change or
// new index compared to the previous i indices.)
// 0 = Mercury
// 1 = Venus
// *2 = Earth
// 3 = Mars
// 4 = Jupiter
// 5 = Saturn
// 6 = Uranus
// 7 = Neptune
// 8 = Pluto
// *9 = Moon
// 10 = Sun
// *11 = Solar-System barycenter
// *12 = Earth-Moon barycenter
// *13 = nutation angles
// *14 = lunar librations
// *15 = Moon (geocentric)
}
//
// If we want something other than coordinates relative to
// the solar system barycenter, subtract coordinates of
// the reference body (supplied by the calling routine via
// the coords->center index in the new indexing scheme)
// from all coordinates except nutation angles (which as a
// side effect avoids dealing with the 4 components in
// that special case), libration angles, and geocentric
// lunar position
//
if ( !coords->bary )
{
if ( 0 <= coords->center && coords->center <= 12 )
{
for ( i = 0; i < 13; i++ )
{
if ( i != coords->center )
{
for ( j = 0; j < 6; j++ )
coords->pv[i][j] -= coords->pv[coords->center][j];
}
else
{
for ( j = 0; j < 6; j++ )
coords->pv[coords->center][j] = 0.;
}
}
}
else
{
fprintf( stderr, "ephcom_get_coords: coords->center = %d is outside the valid range from 0 to 12.\n", coords->center );
exit( EXIT_FAILURE );
}
}
if ( !coords->km ) // Calculate AU, not kilometers
{
for ( i = 0; i < 15; i++ )
{
// Skip over nutations (which as a side effect
// avoids dealing with the 4 components in that
// special case) and librations.
if ( i == 13 )
i = 15;
for ( j = 0; j < 6; j++ )
coords->pv[i][j] /= header->au;
}
}
}
}
return ( retval );
}
//! Interpolate position and velocity (or nutation or libration angles
//! and their time derivatives) at a time point (converted to
//! Chebyshev coordinate in range [-1,1]) using JPL Chebyshev
//! coefficients supplied for one solar system JPL "body" index, where
//! the JPL "bodies" are identified as follows:
//! <table border>
//! <tr> <td><b>Index</b></td> <td><b>Identification</b></td> </tr>
//! <tr> <td>0</td> <td>Mercury</td> </tr>
//! <tr> <td>1</td> <td>Venus</td> </tr>
//! <tr> <td>2</td> <td>Earth-Moon Barycenter</td> </tr>
//! <tr> <td>3</td> <td>Mars</td> </tr>
//! <tr> <td>4</td> <td>Jupiter</td> </tr>
//! <tr> <td>5</td> <td>Saturn</td> </tr>
//! <tr> <td>6</td> <td>Uranus</td> </tr>
//! <tr> <td>7</td> <td>Neptune</td> </tr>
//! <tr> <td>8</td> <td>Pluto</td> </tr>
//! <tr> <td>9</td> <td>Moon (Geocentric)</td> </tr>
//! <tr> <td>10</td> <td>Sun</td> </tr>
//! <tr> <td>11</td> <td>Nutation angles</td> </tr>
//! <tr> <td>12</td> <td>Lunar Libration angles</td> </tr>
//! </table>
//!
//! @param maxcoeffs [INPUT ONLY]Maximum number of Chebyshev
//! components possible.
//! @param x [INPUT ONLY]Value of x over [-1,1] for Chebyshev
//! interpolation.
//! @param span [INPUT ONLY]Span of subinterval in the time coordinate
//! used for the time derivatives (velocity or radians per second for
//! the angular coordinates).
//! @param y [INPUT ONLY]Pointer to an array of required Chebyshev
//! coefficients for a particular JPL "body".
//! @param ncoords [INPUT ONLY]Total number of coordinates to
//! interpolate for a particular JPL "body". This quantity is 3
//! except for nutation where it is two.
//! @param ncoeffs [INPUT ONLY]Number of Chebyshev coefficients per
//! coordinate.
//! @param pv [OUTPUT ONLY]Pointer to an array to hold interpolated
//! positions (or angles) in 1st half, interpolated velocity (or angle
//! time derivatives) in 2nd half for a particular JPL "body".
//!
static inline void
ephcom_cheby( int maxcoeffs, double x, double span, double *y,
int ncoords, int ncoeffs, double *pv )
{
int i, j;
static double twox;
static double *pc, *vc; // Position and velocity polynomial coefficients.
static double lastx = 2.0; // x from last call; initialize to impossible value
static int init = 1; // Need to initialize pc[] and vc[]
//
// Allocate position and velocity Chebyshev coefficients.
//
if ( init )
{
// It is extremely convenient to "permanently" malloc space for
// pc and vc like this. Ideally, one would have a special call
// to ephcom_cheby to free pc and vc or else malloc and free the
// space outside the routine, but these changes are more trouble
// than they are worth so we will have to pay the price of
// valgrind complaining about that unfreed space.
if ( ( pc = (double *) malloc( maxcoeffs * sizeof ( double ) ) ) == NULL )
{
fprintf( stderr, "ephcom_cheby: Cannot malloc pc" );
exit( EXIT_FAILURE );
}
if ( ( vc = (double *) malloc( maxcoeffs * sizeof ( double ) ) ) == NULL )
{
fprintf( stderr, "ephcom_cheby: Cannot malloc vc" );
exit( EXIT_FAILURE );
}
init = 0;
}
//
// This need only be called once for each Julian Date,
// saving a lot of time initializing polynomial coefficients.
//
if ( lastx != x )
{
lastx = x;
twox = x + x; // For Chebyshev recursion
//
// Initialize position polynomial coefficients
//
pc[0] = 1.0; // Chebyshev T[0](x) = 1
pc[1] = x; // Chebyshev T[1](x) = x
for ( i = 2; i < maxcoeffs; i++ )
{
pc[i] = twox * pc[i - 1] - pc[i - 2];
// Resolve bug with gcc generating -0.0 (also makes
// the smallest represented number equal to zero).
//
if ( pc[i] * pc[i] == 0.0 )
{
pc[i] = 0.0;
}
}
//
// Initialize derivative polynomial coefficients
//
vc[0] = 0.0; // d(1)/dx = 0
vc[1] = 1.0; // d(x)/dx = 1
vc[2] = twox + twox; // d(2x^2 - 1)/dx = 4x
for ( i = 3; i < maxcoeffs; i++ )
{
vc[i] = twox * vc[i - 1] + pc[i - 1] + pc[i - 1] - vc[i - 2];
}
}
//
// Interpolate to get position for each component
//
for ( i = 0; i < ncoords; i++ ) // Once each for x, y, and z
{
pv[i] = 0.0;
for ( j = ncoeffs - 1; j >= 0; j-- )
{
pv[i] += pc[j] * y[i * ncoeffs + j];
}
}
//
// Interpolate velocity (first derivative)
//
for ( i = 0; i < ncoords; i++ )
{
pv[ncoords + i] = 0.0;
for ( j = ncoeffs - 1; j >= 0; j-- )
{
pv[ncoords + i] += vc[j] * y[i * ncoeffs + j];
}
pv[ncoords + i] *= 2.0 / span;
}
}
//! Convert Julian Day to calendar date and time. From pp. 604, 606
//! in the Explanatory Supplement to the Astronomical Almanac.
//!
//! @param tjd [IN ONLY]Double-precision Julian Day number.
//! @param idate [OUT ONLY] integer array of 6 values which upon
//! return will contain the integer year, month, day, hour, minute,
//! and second corresponding to tjd.
//! @param calendar_type [IN ONLY]Integer value which controls the
//! kind of calendar used for the transformation: -1=Julian;
//! 0=automatic; 1=Gregorian. If automatic, use Julian calendar for
//! dates before 15 October 1582.
//!
static void
ephcom_jd2cal( double tjd, int idate[6], int calendar_type )
{
int ihour, imin, isec;
int j;
// From Explanatory Supplement to Astronomical Almanac, pp. 604, 606
int I, J, K, L, N, D, M, Y;
tjd += 0.5 + 0.5 / 86400.0; // Round to nearest second
j = tjd; // Integer Julian Day
tjd = ( tjd - j ) * 24.0;
ihour = tjd;
tjd = ( tjd - ihour ) * 60.0;
imin = tjd;
tjd = ( tjd - imin ) * 60.0;
isec = tjd;
//
// Julian calendar. Explanatory Supplement to Astronomical Alamanac, p. 606.
// If automatic, use Julian calendar for dates before 15 October 1582.
//
if ( calendar_type == -1 || ( calendar_type == 0 && j <= 2299160 ) )
{
J = j + 1402;
K = ( J - 1 ) / 1461;
L = J - 1461 * K;
N = ( L - 1 ) / 365 - L / 1461;
I = L - 365 * N + 30;
J = ( 80 * I ) / 2447;
D = I - ( 2447 * J ) / 80;
I = J / 11;
M = J + 2 - 12 * I;
Y = 4 * K + N + I - 4716;
}
//
// Gregorian calendar.
//
else // Explanatory Supplement to Astronomical Almanac, p. 604
{
L = j + 68569;
N = ( 4 * L ) / 146097;
L = L - ( 146097 * N + 3 ) / 4;
I = ( 4000 * ( L + 1 ) ) / 1461001;
L = L - ( 1461 * I ) / 4 + 31;
J = ( 80 * L ) / 2447;
D = L - ( 2447 * J ) / 80;
L = J / 11;
M = J + 2 - 12 * L;
Y = 100 * ( N - 49 ) + I + L;
}
idate[0] = Y;
idate[1] = M;
idate[2] = D;
idate[3] = ihour;
idate[4] = imin;
idate[5] = isec;
}
//! Convert calendar date and time to JD. From pp. 604, 606 in the
//! Explanatory Supplement to the Astronomical Almanac.
//!
//! @param idate [IN ONLY] integer array of 6 values which contains
//! the integer year, month, day, hour, minute, and second.
//! @param calendar_type [IN ONLY]Integer value which controls the
//! kind of calendar used for the transformation: -1=Julian;
//! 0=automatic; 1=Gregorian. If automatic, use Julian calendar for
//! dates before 15 October 1582.
//! @returns double-precision Julian Day number corresponding to idate.
//!
double
ephcom_cal2jd( int idate[6], int calendar_type )
{
double tjd;
int jd;
//
// Convert hours, minutes, seconds to fractional JD.
//
tjd = ( idate[3] + ( idate[4] + idate[5] / 60.0 ) / 60.0 ) / 24.0 - 0.5;
//
// Julian calendar. Explanatory Supplement to Astronomical Alamanac, p. 606.
// If automatic, use Julian calendar for dates before 15 October 1582.
//
if ( calendar_type == -1 ||
( calendar_type == 0 &&
( idate[0] < 1582 || // Before 1582
( idate[0] == 1582 &&
( idate[1] < 10 || // Before October 1582
( idate[1] == 10 && idate[2] < 15 ) ) ) ) ) ) // Before 15 October 1582
{
jd = 367 * idate[0] -
( 7 * ( idate[0] + 5001 + ( idate[1] - 9 ) / 7 ) ) / 4 +
( 275 * idate[1] ) / 9 +
idate[2] + 1729777;
}
//
// Gregorian calendar.
//
else // Explanatory Supplement to Astronomical Almanac, p. 604
{
jd = ( 1461 * ( idate[0] + 4800 + ( idate[1] - 14 ) / 12 ) ) / 4 +
( 367 * ( idate[1] - 2 - 12 * ( ( idate[1] - 14 ) / 12 ) ) ) / 12 -
( 3 * ( ( idate[0] + 4900 + ( idate[1] - 14 ) / 12 ) / 100 ) ) / 4 +
idate[2] - 32075;
}
//
// Return value is whole JD number plus fractional JD number.
//
tjd += (double) jd;
return ( tjd );
}
//! If Julian date is close to an integer + 0.5, return that exact
//! "half" value. Use of this routine makes the code more robust for
//! an early version of de422 (since corrected) which had numerical
//! noise in its half days.
//!
//! @param time [IN ONLY]Value of the Julian date which should be
//! exactly half integral.
//! @returns exactly half integral Julian date closest to time if
//! input time close to half-integral. If input time is not close
//! to half-integral the routine returns the unmodified input time.
//!
static double
ephcom_exact_time( double time )
{
double exact_half_time = ( time >= 0. ) ? (double) ( (int) time + 0.5 ) : (double) ( (int) time - 0.5 );
if ( IF_SAME_DATE( time, exact_half_time ) )
return exact_half_time;
else
return time;
}
//! Split time into an integer part and a positive remainder in the
//! semi-open range [0., 1.).
//!
//! @param time [IN ONLY]time value to be split.
//! @param integral_time [OUT ONLY]Pointer to a double value which
//! upon return will contain the integral part of the split time.
//! @returns remainder of the split time in the semi-open range [0., 1.).
//!
static double
ephcom_split( double time, double * integral_time )
{
double retval = modf( time, integral_time );
if ( retval < 0. )
{
retval += 1.;
*integral_time -= 1.;
}
return retval;
}
ephcom.h 0 → 100755
View file @ b2540417
//! @file
//! Header information for the ephcom library.
//!
// Copyright (C) 1994-2004 Paul Hardy
// Copyright (C) 2011 Alan W. Irwin
//
// This file is part of the timeephem software project.
//
// timeephem is free software; you can redistribute it and/or modify
// it under the terms of the GNU Library General Public License as published
// by the Free Software Foundation; version 2 of the License.
//
// timeephem is distributed in the hope that it will be useful,
// but WITHOUT ANY WARRANTY; without even the implied warranty of
// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
// GNU Library General Public License for more details.
//
// You should have received a copy of the GNU Library General Public License
// along with timeephem; if not, write to the Free Software
// Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301 USA
// Note that this software is not a product of the Jet Propulsion
// Laboratory; it just uses and supports their ASCII and binary
// ephemeris files. Please don't mail JPL concerning any bugs.
// Send bug reports or suggestions to airwin@users.sourceforge.net instead.
#ifndef __EPHCOM_H__
#define __EPHCOM_H__
// Set up for dealing with function visibility issues.
#include "ephcomdll.h"
#define EPHCOM_VERSION "1.0"
#define EPHCOM_MAXLINE 128 // Maximum # characters to allow in input line
#define EPHCOM_MAXTTL 84 // Maximum # characters of information in ttl[0-3]
#define EPHCOM_MINJD -999999999.5
#define EPHCOM_MAXJD 999999999.5
// Objects for pleph() ntarget and ncenter parameters.
#define EPHCOM_MERCURY 1
#define EPHCOM_VENUS 2
#define EPHCOM_EARTH 3
#define EPHCOM_MARS 4
#define EPHCOM_JUPITER 5
#define EPHCOM_SATURN 6
#define EPHCOM_URANUS 7
#define EPHCOM_NEPTUNE 8
#define EPHCOM_PLUTO 9
#define EPHCOM_MOON 10 // Moon, relative to Solar System center
#define EPHCOM_SUN 11
#define EPHCOM_SSBARY 12 // Solar System Barycenter
#define EPHCOM_EMBARY 13 // Earth-Moon Barycenter
#define EPHCOM_NUTATION 14
#define EPHCOM_LIBRATION 15
#define EPHCOM_GEOMOON 16 // Original Lunar Ephemeris coordinates
#define EPHCOM_OBSERVER 17 // User-defined observer position
#define EPHCOM_NUMOBJECTS 17 // Allocate memory for 17 solar sys objs
//! This structure holds all the information contained in a JPLEPH header.
//! When an ASCII or binary header is read, this structure is populated.
//! Fill out this structure before writing an ASCII or binary header, and
//! before performing any interpolations.
//!
#ifdef __cplusplus
extern "C"{
#endif
typedef struct
{
//! block size, in first line of ASCII header.
int ksize;
//! Number of Chebyshev coefficients in data blocks.
int ncoeff;
//! Hold up to 14*6=EPHCOM_MAXTTL characters + "\n" + null.
char ttl[3][EPHCOM_MAXTTL + 2];
//! Number of assigned in cnam.
int ncon;
//! Hold up to 400 6-character names ending with null.
char cnam[400][7];
//! Number of values for cval, to compare with ncon.
int nval;
//! Constant values, corresponding to cnam names.
double cval[400];
//! Astronomical unit in km.
double au;
//! Earth-Moon mass ratio.
double emrat;
//! Speed of light, km/sec.
double clight;
//! Ephemeris number.
int numde;
//! Lunar ephemeris number (can be same # as numde).
int numle;
//! Start Julian day number, stop Julian day number, and step size (in days).
double ss[3];
//! Index pointers into Chebyshev coefficients.
int ipt[12][3];
//! Libration pointer in a block.
int lpt[3];
//! Maximum Chebyshev coefficients for a body.
int maxcheby;
} ephcom_Header;
//! This struct holds all interpolated positions of planets, Sun, and Moon
//! at a given time. All of the information available from interpolation
//! at a given point in time is computed at once and preserved here.
//!
//! To populate this structure, have the ephemeris file open, and set:
//!
//! km, seconds, bary, et2[0], and et2[1] in the ephcom_Coords struct whose
//! pointer is an argument to ephcom_get_coords().
//!
//! Then call ephcom_get_coords() to get all coordinates, then call
//! ephcom_pleph() for each desired (ntarget,ncenter) combination.
//! See testeph.c for an example. Note that unlike JPL's PLEPH()
//! subroutine, you cannot call ephcom_pleph() without first initializing
//! the pv[] array in ephcom_get_coords().
//!
//! The first index of pv is
//! interpreted as follows (note the offset by one compared to the
//! interpretation of the index arguments to ephcom_pleph()):
//! <table border>
//! <tr> <td><b>Index</b></td> <td><b>Identification</b></td> </tr>
//! <tr> <td>0</td> <td>Mercury</td> </tr>
//! <tr> <td>1</td> <td>Venus</td> </tr>
//! <tr> <td>2</td> <td>Earth</td> </tr>
//! <tr> <td>3</td> <td>Mars</td> </tr>
//! <tr> <td>4</td> <td>Jupiter</td> </tr>
//! <tr> <td>5</td> <td>Saturn</td> </tr>
//! <tr> <td>6</td> <td>Uranus</td> </tr>
//! <tr> <td>7</td> <td>Neptune</td> </tr>
//! <tr> <td>8</td> <td>Pluto</td> </tr>
//! <tr> <td>9</td> <td>Moon</td> </tr>
//! <tr> <td>10</td> <td>Sun</td> </tr>
//! <tr> <td>11</td> <td>Solar System Barycenter</td> </tr>
//! <tr> <td>12</td> <td>Earth-Moon Barycenter</td> </tr>
//! <tr> <td>13</td> <td>Nutation Angles</td> </tr>
//! <tr> <td>14</td> <td>Libration Angles</td> </tr>
//! <tr> <td>15</td> <td>Moon (Geocentric)</td> </tr>
//! <tr> <td>16</td> <td>Possible user-defined coordinates</td> </tr>
//! </table>
//!
//! There are some extra entries at the end, compared to JPL's PLEPH():
//!
//! pv[15][] - preserves the unmodified lunar ephemeris coordinates.
//! These coordinates are never offset by center, so that
//! their full precision is maintained.
//! pv[16][] - start of possible user-defined coordinates.
//! These coordinates are offset by center.
//!
typedef struct
{
//! 1 = positions in km; 0 = positions in AU.
int km;
//! 1 = timescale is seconds; 0 = timescale is days.
int seconds;
//! 1 = Barycentric coordinates; 0 = adjust for center.
int bary;
//! object to use as center (instead of SSBARY).
int center;
//! 0 = raw JPL ephemeris coordinates. Note: none of the supplied routines read or modify the coordtype value.
int coordtype;
//! Julian Day of interpolation. For best precision, et2[0] should be an exact integral or exact half-integral number of days while et2[1] should be a correction to et2[0] between 0. and 1.
double et2[2];
//! x, y, z Position & Velocity. The first index of pv is interpreted as in the above table.
double pv[EPHCOM_NUMOBJECTS][6];
} ephcom_Coords;
// Useful macro for Julian date comparison.
// JPL ephemeris Julian dates (so far) range from 6.e5 (3000 BC) to 2.8e6 (3000 AD). So
// double precision (64-bit floating point) should be able to represent a date to within
// ~ 1.e-15*2.8e6 = 2.8e-9 days (or 0.24 ms). Make criterion ~100 times that value since
// all JPL ephemerides up to now have dates which are offset by 0.5 from an integer so
// that a criterion of 0.25 days would probably work.
#define JULIAN_DATE_CRITERION ( 3.e-7 )
// Need this logic to compare dates rather than exact equalities because
// (for DE422 at least) rounding errors have crept into the dates.
#define IF_SAME_DATE( a, b ) ( fabs( a - b ) <= JULIAN_DATE_CRITERION )
// Here is where the public API for libephcom is described.
// Read a JPL Ephemeris ASCII header from the FILE pointed to by the
// infp argument and store and return values in the ephcom_Header
// struct pointed to by the header argument. Write any errors to
// stderr.
EPHCOMDLLIMPEXP void
ephcom_readascii_header( FILE * infp, ephcom_Header *header );
//
// Read a block of data coefficients from a JPL ASCII ephemeris file.
// Returns number of coefficients read, 0 at EOF.
//
EPHCOMDLLIMPEXP int
ephcom_readascii_block(
FILE * infp,
ephcom_Header *header,
double *datablock );
//
// Read a JPL Ephemeris header in binary format. Store values in
// an ephcom_Header struct.
//
EPHCOMDLLIMPEXP void
ephcom_readbinary_header( FILE * infp, ephcom_Header *header );
//
// Read a JPL Ephemeris data block in binary format.
//
// This is the only routine in this library that accesses a file
// as a direct access file, with a specified block number. The
// block number ranges from 0 on up (starting at first data block,
// after the 2 header blocks). Returns the number of coefficients
// read, or 0 at EOF.
//
EPHCOMDLLIMPEXP int
ephcom_readbinary_block(
FILE *infp, // File pointer for direct access file
ephcom_Header *header, // header struct, already filled in
int blocknum, // Data block number, starting with 0
double *datablock // returned coefficient data block
);
//
// Write header information in ASCII format.
//
EPHCOMDLLIMPEXP void
ephcom_writeascii_header( FILE * outfp, ephcom_Header *header );
//
// Write coefficient block information in ASCII format.
//
EPHCOMDLLIMPEXP void
ephcom_writeascii_block(
FILE * outfp,
ephcom_Header *header,
int blocknum,
double *datablock );
//
// Write a JPL Ephemeris header in binary format.
//
EPHCOMDLLIMPEXP void
ephcom_writebinary_header( FILE *outfp, ephcom_Header *header );
//
// Write a block of data coefficients in JPL binary file format.
//
EPHCOMDLLIMPEXP void
ephcom_writebinary_block(
FILE * outfp,
ephcom_Header *header,
int blocknum,
double *datablock );
//
// ephcom_parse_block() - Parse a binary block of data. Warning: verbose!
// Writes parsed output to file pointer outfp.
//
EPHCOMDLLIMPEXP void
ephcom_parse_block(
FILE * outfp,
ephcom_Header *header,
double *datablock );
//
// Read in a double precision value from the given file with bytes swapped
// if necessary to match host order (Little- or DEC- Endian). On Intel 80x86
// the bytes will get swapped, on Motorola or SPARC they won't.
//
EPHCOMDLLIMPEXP double
ephcom_indouble( FILE *infp );
//
// Read in an integer (4--byte) value to the given file with bytes swapped
// if necessary to match host order (Little- or DEC- Endian). On Intel 80x86
// the bytes will get swapped, on Motorola or SPARC they won't.
//
EPHCOMDLLIMPEXP int
ephcom_inint( FILE *infp );
//
// Planetary Ephemeris. Takes coordinates already calculated in
// coords structure and converts to vectors and vector dot in testr[].
// Bodies start at 1 for Mercury, to match the JPL PLEPH() numbering.
// Values for ntarg and ncntr correspond to locations ntarg-1 and
// ncntr-1 in coords->pv[].
//
EPHCOMDLLIMPEXP void
ephcom_pleph( ephcom_Coords *coords, int ntarg, int ncntr, double *r );
//
// ephcom_get_coords() - Interpolate positions and velocities at given time.
//
EPHCOMDLLIMPEXP int
ephcom_get_coords( FILE * infp,
ephcom_Header *header,
ephcom_Coords *coords,
double *datablock );
//
// ephcom_cal2jd() - convert calendar date and time to JD.
//
// idate: integer year, month, day, hour, minute, second
// calendar_type: -1=Julian; 0=Automatic; 1=Gregorian
// return value: double precision Julian Day of idate[]
//
// From pp. 604, 606 in the Explanatory Supplement to the Astronomical Almanac.
//
EPHCOMDLLIMPEXP double
ephcom_cal2jd( int idate[6], int calendar_type );
#ifdef __cplusplus
}
#endif
#endif // __EPHCOM_H__
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