Replace shao.py

csst_mci_sim/support/shao.py

 from ctypes import *
 
-#def checkInputList(input_list, n):
-#    if type(input_list) != type([1, 2, 3]):
-#        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 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 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 type(input_x) != type(1.1):
-#        raise TypeError("Parameter 8 is not double!", input_x)
-#    if type(input_y) != type(1.1):
-#        raise TypeError("Parameter 9 is not double!", input_y)
-#    if type(input_z) != type(1.1):
-#        raise TypeError("Parameter 10 is not double!", input_z)
-#    if type(input_vx) != type(1.1):
-#        raise TypeError("Parameter 11 is not double!", input_vx)
-#    if type(input_vy) != type(1.1):
-#        raise TypeError("Parameter 12 is not double!", input_vy)
-#    if type(input_vz) != type(1.1):
-#        raise TypeError("Parameter 13 is not double!", input_vz)
-    
-    #Convert km -> m
+
+
+    # Convert km -> m
     input_x = input_x*1000.0 
     input_y = input_y*1000.0 
     input_z = input_z*1000.0
@@ -129,6 +98,5 @@ def onOrbitObsPosition(path, input_ra_list, input_dec_list, input_pmra_list, inp
             raise RuntimeError("Calculate error!")
         output_ra_list.append(output_ra.value)
         output_dec_list.append(output_dec.value)
-    
+
     return output_ra_list, output_dec_list
-    
\ No newline at end of file