from ctypes import * import numpy as np try: import importlib.resources as pkg_resources except ImportError: # Try backported to PY<37 'importlib_resources' import importlib_resources as pkg_resources def checkInputList(input_list, n): if not isinstance(input_list, list): raise TypeError("Input type is not list!", input_list) for i in input_list: if type(i) != type(1.1): if 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 on_orbit_obs_position(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, lib_path=None): #Check input parameters if not isinstance(input_nstars, int): 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 not isinstance(input_x, float): raise TypeError("Parameter 8 is not double!", input_x) if not isinstance(input_y, float): raise TypeError("Parameter 9 is not double!", input_y) if not isinstance(input_z, float): raise TypeError("Parameter 10 is not double!", input_z) if not isinstance(input_vx, float): raise TypeError("Parameter 11 is not double!", input_vx) if not isinstance(input_vy, float): raise TypeError("Parameter 12 is not double!", input_vy) if not isinstance(input_vz, float): raise TypeError("Parameter 13 is not double!", input_vz) #Convert km -> m input_x = input_x*1000.0 input_y = input_y*1000.0 input_z = input_z*1000.0 input_vx = input_vx*1000.0 input_vy = input_vy*1000.0 input_vz = input_vz*1000.0 if not isinstance(input_date_str, str): raise TypeError("Parameter 15 is not string!", input_date_str) else: input_date_str = input_date_str.strip() if not (input_date_str[4]=="-" and input_date_str[7]=="-"): raise TypeError("Parameter 15 format error (1)!", input_date_str) else: tmp = input_date_str.split("-") if len(tmp) != 3: 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) if not (input_month>=1 and input_month<=12): 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) if not isinstance(input_time_str, str): raise TypeError("Parameter 16 is not string!", input_time_str) else: input_time_str = input_time_str.strip() if not (input_time_str[2]==":" and input_time_str[5]==":"): raise TypeError("Parameter 16 format error (1)!", input_time_str) else: tmp = input_time_str.split(":") if len(tmp) != 3: 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) if not (input_minute>=0 and input_minute<=59): 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) #Inital dynamic lib # shao = cdll.LoadLibrary(lib_path) with pkg_resources.path('ObservationSim.Astrometry.lib', "libshao.so") as lib_path: shao = cdll.LoadLibrary(lib_path) 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, \ POINTER(c_double), POINTER(c_double) ] output_ra_list = list() output_dec_list = list() for i in range(input_nstars): input_ra = c_double(input_ra_list[i]) input_dec = c_double(input_dec_list[i]) input_pmra = c_double(input_pmra_list[i]) input_pmdec = c_double(input_pmdec_list[i]) input_rv = c_double(input_rv_list[i] * 3600.) # Convert from km/s to km/h input_parallax = c_double(input_parallax_list[i]) p3 = d3(input_x, input_y, input_z) v3 = d3(input_vx, input_vy, input_vz) input_year_c = c_int(input_year) input_month_c = c_int(input_month) input_day_c = c_int(input_day) input_hour_c = c_int(input_hour) input_minute_c = c_int(input_minute) input_second_c = c_double(input_second) 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, \ byref(output_ra), byref(output_dec)) if rs != 0: raise RuntimeError("Calculate error!") output_ra_list.append(output_ra.value) output_dec_list.append(output_dec.value) return np.array(output_ra_list), np.array(output_dec_list)