1 /*
2  * Unit Solar
3  *           Author:  Dr TS Kelso
4  * Original Version:  1990 Jul 29
5  * Current Revision:  1999 Nov 27
6  *          Version:  1.30
7  *        Copyright:  1990-1999, All Rights Reserved
8  *
9  *   Ported to C by: Neoklis Kyriazis  April 1 2001
10  */
11 
12 #include "sgp4sdp4.h"
13 
14 /* Calculates solar position vector */
15 void
Calculate_Solar_Position(double _time,vector_t * solar_vector)16 Calculate_Solar_Position(double _time, vector_t *solar_vector)
17 {
18   double mjd,year,T,M,L,e,C,O,Lsa,nu,R,eps;
19 
20   mjd = _time - 2415020.0;
21   year = 1900 + mjd/365.25;
22   T = (mjd + Delta_ET(year)/secday)/36525.0;
23   M = Radians(Modulus(358.47583 + Modulus(35999.04975*T,360.0)
24 		      - (0.000150 + 0.0000033*T)*Sqr(T),360.0));
25   L = Radians(Modulus(279.69668 + Modulus(36000.76892*T,360.0)
26 		      + 0.0003025*Sqr(T),360.0));
27   e = 0.01675104 - (0.0000418 + 0.000000126*T)*T;
28   C = Radians((1.919460 - (0.004789 + 0.000014*T)*T)*sin(M)
29 	      + (0.020094 - 0.000100*T)*sin(2*M) + 0.000293*sin(3*M));
30   O = Radians(Modulus(259.18 - 1934.142*T,360.0));
31   Lsa = Modulus(L + C - Radians(0.00569 - 0.00479*sin(O)),twopi);
32   nu = Modulus(M + C,twopi);
33   R = 1.0000002*(1 - Sqr(e))/(1 + e*cos(nu));
34   eps = Radians(23.452294 - (0.0130125 + (0.00000164 -
35 		0.000000503*T)*T)*T + 0.00256*cos(O));
36   R = AU*R;
37   solar_vector->x = R*cos(Lsa);
38   solar_vector->y = R*sin(Lsa)*cos(eps);
39   solar_vector->z = R*sin(Lsa)*sin(eps);
40   solar_vector->w = R;
41 } /*Procedure Calculate_Solar_Position*/
42 
43 /*------------------------------------------------------------------*/
44 
45 /* Calculates stellite's eclipse status and depth */
46 int
Sat_Eclipsed(vector_t * pos,vector_t * sol,double * depth)47 Sat_Eclipsed(vector_t *pos, vector_t *sol, double *depth)
48 {
49   double sd_sun, sd_earth, delta;
50   vector_t Rho, earth;
51 
52   /* Determine partial eclipse */
53   sd_earth = ArcSin(xkmper/pos->w);
54   Vec_Sub(sol,pos,&Rho);
55   sd_sun = ArcSin(__sr__/Rho.w);
56   Scalar_Multiply(-1,pos,&earth);
57   delta = Angle(sol,&earth);
58   *depth = sd_earth - sd_sun - delta;
59   if( sd_earth < sd_sun )
60     return( 0 );
61   else
62     if( *depth >= 0 )
63       return( 1 );
64     else
65       return( 0 );
66 
67 } /*Function Sat_Eclipsed*/
68 
69 /*------------------------------------------------------------------*/
70