Replace shao.py (6ceaf0e0) · Commits · csst-sims / csst_mci_sim

csst_mci_sim/support/shao.py

+88 −42

Original line number	Diff line number	Diff line
		from ctypes import *


		def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, input_pmdec_list, input_rv_list, \
		input_parallax_list, input_nstars, input_x, input_y, input_z, input_vx, input_vy, \
		# def checkInputList(input_list, n):
		# if isinstance(type(input_list), list):
		# # if type(input_list) != type([1, 2, 3]):
		# raise TypeError("Input type is not list!", input_list)
		# for i in input_list:
		# if isinstance(type(i), float): # type(i) != type(1.1):
		# if isinstance(type(i), int): # type(i) != type(1):
		# raise TypeError(
		# "Input list's element is not float or int!", input_list)
		# if len(input_list) != n:
		# raise RuntimeError(
		# "Length of input list is not equal to stars' number!", input_list)


		def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, input_pmdec_list, input_rv_list,
		input_parallax_list, input_nstars, input_x, input_y, input_z, input_vx, input_vy,
		input_vz, input_epoch, input_date_str, input_time_str):
		# Check input parameters
		if isinstance(type(input_nstars), type(1)): # type(input_nstars) != type(1):
		raise TypeError("Parameter 7 is not int!", input_nstars)

		# checkInputList(input_ra_list, input_nstars)
		# checkInputList(input_dec_list, input_nstars)
		# checkInputList(input_pmra_list, input_nstars)
		# checkInputList(input_pmdec_list, input_nstars)
		# checkInputList(input_rv_list, input_nstars)
		# checkInputList(input_parallax_list, input_nstars)
		#
		# if isinstance(type(input_x), type(1.1)): # type(input_x) != type(1.1):
		# raise TypeError("Parameter 8 is not double!", input_x)
		# if isinstance(type(input_y), type(1.1)): # type(input_y) != type(1.1):
		# raise TypeError("Parameter 9 is not double!", input_y)
		# if isinstance(type(input_z), type(1.1)): # type(input_z) != type(1.1):
		# raise TypeError("Parameter 10 is not double!", input_z)
		# if isinstance(type(input_vx), type(1.1)): # type(input_vx) != type(1.1):
		# raise TypeError("Parameter 11 is not double!", input_vx)
		# if isinstance(type(input_vy), type(1.1)): # type(input_vy) != type(1.1):
		# raise TypeError("Parameter 12 is not double!", input_vy)
		# if isinstance(type(input_vz), type(1.1)): # type(input_vz) != type(1.1):
		# raise TypeError("Parameter 13 is not double!", input_vz)

		# Convert km -> m
		input_x = input_x*1000.0
		@@ -14,7 +50,8 @@ def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, inp
		input_vy = input_vy*1000.0
		input_vz = input_vz*1000.0

		if type(input_date_str) != type("2025-03-05"):
		if isinstance(type(input_date_str), type("2025-03-05")):
		# type(input_date_str) != type("2025-03-05"):
		raise TypeError("Parameter 15 is not string!", input_date_str)
		else:
		input_date_str = input_date_str.strip()
		@@ -23,18 +60,23 @@ def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, inp
		else:
		tmp = input_date_str.split("-")
		if len(tmp) != 3:
		raise TypeError("Parameter 15 format error (2)!", input_date_str)
		raise TypeError(
		"Parameter 15 format error (2)!", input_date_str)
		input_year = int(tmp[0])
		input_month = int(tmp[1])
		input_day = int(tmp[2])
		if not (input_year >= 1900 and input_year <= 2100):
		raise TypeError("Parameter 15 year range error [1900 ~ 2100]!", input_year)
		raise TypeError(
		"Parameter 15 year range error [1900 ~ 2100]!", input_year)
		if not (input_month >= 1 and input_month <= 12):
		raise TypeError("Parameter 15 month range error [1 ~ 12]!", input_month)
		raise TypeError(
		"Parameter 15 month range error [1 ~ 12]!", input_month)
		if not (input_day >= 1 and input_day <= 31):
		raise TypeError("Parameter 15 day range error [1 ~ 31]!", input_day)
		raise TypeError(
		"Parameter 15 day range error [1 ~ 31]!", input_day)

		if type(input_time_str) != type("20:15:15.15"):
		if isinstance(type(input_time_str), type("20:15:15.15")):
		# type(input_time_str) != type("20:15:15.15"):
		raise TypeError("Parameter 16 is not string!", input_time_str)
		else:
		input_time_str = input_time_str.strip()
		@@ -43,16 +85,20 @@ def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, inp
		else:
		tmp = input_time_str.split(":")
		if len(tmp) != 3:
		raise TypeError("Parameter 16 format error (2)!", input_time_str)
		raise TypeError(
		"Parameter 16 format error (2)!", input_time_str)
		input_hour = int(tmp[0])
		input_minute = int(tmp[1])
		input_second = float(tmp[2])
		if not (input_hour >= 0 and input_hour <= 23):
		raise TypeError("Parameter 16 hour range error [0 ~ 23]!", input_hour)
		raise TypeError(
		"Parameter 16 hour range error [0 ~ 23]!", input_hour)
		if not (input_minute >= 0 and input_minute <= 59):
		raise TypeError("Parameter 16 minute range error [0 ~ 59]!", input_minute)
		raise TypeError(
		"Parameter 16 minute range error [0 ~ 59]!", input_minute)
		if not (input_second >= 0 and input_second < 60.0):
		raise TypeError("Parameter 16 second range error [0 ~ 60)!", input_second)
		raise TypeError(
		"Parameter 16 second range error [0 ~ 60)!", input_second)
		# Inital dynamic lib

		import os
		@@ -64,10 +110,10 @@ def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, inp
		shao.onOrbitObs.restype = c_int

		d3 = c_double * 3
		shao.onOrbitObs.argtypes = [c_double, c_double, c_double, c_double, c_double, c_double, \
		c_int, c_int, c_int, c_int, c_int, c_double, \
		c_double, POINTER(d3), POINTER(d3), \
		c_int, c_int, c_int, c_int, c_int, c_double, \
		shao.onOrbitObs.argtypes = [c_double, c_double, c_double, c_double, c_double, c_double,
		c_int, c_int, c_int, c_int, c_int, c_double,
		c_double, POINTER(d3), POINTER(d3),
		c_int, c_int, c_int, c_int, c_int, c_double,
		POINTER(c_double), POINTER(c_double)]
		output_ra_list = list()
		output_dec_list = list()
		@@ -89,10 +135,10 @@ def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, inp
		DAT = c_double(37.0)
		output_ra = c_double(0.0)
		output_dec = c_double(0.0)
		rs = shao.onOrbitObs(input_ra, input_dec, input_parallax, input_pmra, input_pmdec, input_rv, \
		input_year_c, input_month_c, input_day_c, input_hour_c, input_minute_c, input_second_c, \
		DAT, byref(p3), byref(v3), \
		input_year_c, input_month_c, input_day_c, input_hour_c, input_minute_c, input_second_c, \
		rs = shao.onOrbitObs(input_ra, input_dec, input_parallax, input_pmra, input_pmdec, input_rv,
		input_year_c, input_month_c, input_day_c, input_hour_c, input_minute_c, input_second_c,
		DAT, byref(p3), byref(v3),
		input_year_c, input_month_c, input_day_c, input_hour_c, input_minute_c, input_second_c,
		byref(output_ra), byref(output_dec))
		if rs != 0:
		raise RuntimeError("Calculate error!")