sdp8.cpp

来自「卫星计算码」· C++ 代码 · 共 239 行

#include <math.h>
#include "norad.h"
#include "norad_in.h"

#define tthmun    params[0]
#define sinio2    params[1]
#define cosio2    params[2]
#define unm5th    params[3]
#define unmth2    params[4]
#define a3cof     params[5]
#define xmdt1     params[6]
#define xgdt1     params[7]
#define xhdt1     params[8]
#define xndt      params[9]
#define edot      params[10]
#define deep_arg  ((deep_arg_t *)( params + 11))

void DLL_FUNC SDP8_init( double *params, const tle_t *tle)
{
   double
         a1, alpha2, ao, b, b1, b2, b3, c0,
         c1, c4, c5, cos2g, d1, d2, d3, d4,
         d5, del1, delo, eeta, eta, eta2,
         pardt1, pardt2, pardt4, po, pom2,
         psim2, r1, temp, theta4, tsi, xndtn;

   /* Recover original mean motion (xnodp) and semimajor axis (aodp) */
   /* from input elements. Calculate ballistic coefficient */
   /* (b term) from input b* drag term */
   a1 = pow( xke / tle->xno, two_thirds);
   deep_arg->cosio = cos(tle->xincl);
   deep_arg->theta2 = deep_arg->cosio*deep_arg->cosio;
   tthmun = deep_arg->theta2*3.-1.;
   deep_arg->eosq = tle->eo*tle->eo;
   deep_arg->betao2 = 1.-deep_arg->eosq;
   deep_arg->betao = sqrt(deep_arg->betao2);
   del1 = ck2*1.5*tthmun/(a1*a1*deep_arg->betao*deep_arg->betao2);
   ao = a1*(1.-del1*(two_thirds*.5+del1*(del1*1.654320987654321+1.)));
   delo = ck2*1.5*tthmun/(ao*ao*deep_arg->betao*deep_arg->betao2);
   deep_arg->aodp = ao/(1.-delo);
   deep_arg->xnodp = tle->xno/(delo+1.);
   b = tle->bstar*2./rho;

   /* Initialization */
   po = deep_arg->aodp*deep_arg->betao2;
   pom2 = 1./(po*po);
   deep_arg->sinio = sin(tle->xincl);
   deep_arg->sing = sin(tle->omegao);
   deep_arg->cosg = cos(tle->omegao);
   temp = tle->xincl*.5;
   sinio2 = sin(temp);
   cosio2 = cos(temp);
   r1 = deep_arg->theta2;
   theta4 = r1*r1;
   unm5th = 1.-deep_arg->theta2*5.;
   unmth2 = 1.-deep_arg->theta2;
   r1 = ae;
   a3cof = -xj3/ck2*(r1*(r1*r1));
   pardt1 = ck2*3.*pom2*deep_arg->xnodp;
   pardt2 = pardt1*ck2*pom2;
   pardt4 = ck4*1.25*pom2*pom2*deep_arg->xnodp;
   xmdt1 = pardt1*.5*deep_arg->betao*tthmun;
   xgdt1 = pardt1*-.5*unm5th;
   xhdt1 = -pardt1*deep_arg->cosio;
   deep_arg->xmdot = deep_arg->xnodp+xmdt1+pardt2*.0625*deep_arg->betao*
               (13.-deep_arg->theta2*78.+theta4*137.);
   deep_arg->omgdot = xgdt1+pardt2*.0625*(7.-deep_arg->theta2*
                     114.+theta4*395.)+pardt4*(3.-deep_arg->theta2*
                     36.+theta4*49.);
   deep_arg->xnodot = xhdt1+(pardt2*.5*(4.-deep_arg->theta2*19.)+pardt4*
      2.*(3.-deep_arg->theta2*7.))*deep_arg->cosio;
   tsi = 1./(po-s);
   eta = tle->eo*s*tsi;
   r1 = eta;
   eta2 = r1*r1;
   psim2 = (r1 = 1./(1.-eta2), fabs(r1));
   alpha2 = deep_arg->eosq+1.;
   eeta = tle->eo*eta;
   r1 = deep_arg->cosg;
   cos2g = r1*r1*2.-1.;
   d5 = tsi*psim2;
   d1 = d5/po;
   d2 = eta2*(eta2*4.5+36.)+12.;
   d3 = eta2*(eta2*2.5+15.);
   d4 = eta*(eta2*3.75+5.);
   b1 = ck2*tthmun;
   b2 = -ck2*unmth2;
   b3 = a3cof*deep_arg->sinio;
   r1 = tsi, r1 *= r1;
   c0 = b*.5*rho*qoms2t*deep_arg->xnodp*deep_arg->aodp*
            (r1*r1)*pow( psim2, 3.5)/sqrt(alpha2);
   r1 = alpha2;
   c1 = deep_arg->xnodp*1.5*(r1*r1)*c0;
   c4 = d1*d3*b2;
   c5 = d5*d4*b3;
   xndt = c1*(eta2*(deep_arg->eosq*34.+3.)+2.+eeta*5.*(eta2+4.)+
     deep_arg->eosq*8.5+d1*d2*b1+c4*cos2g+c5*deep_arg->sing);
   xndtn = xndt/deep_arg->xnodp;
   edot = -two_thirds*xndtn*(1.-tle->eo);

   /* initialize Deep() */
   Deep_dpinit( tle, deep_arg);
#ifdef RETAIN_PERTURBATION_VALUES_AT_EPOCH
   /* initialize lunisolar perturbations: */
   deep_arg->t = 0.;                            /* added 30 Dec 2003 */
   deep_arg->solar_lunar_init_flag = 1;
   Deep_dpper( deep_arg);
   deep_arg->solar_lunar_init_flag = 0;
#endif
} /* End of SDP8() initialization */

void DLL_FUNC SDP8( const double tsince, const tle_t *tle, const double *params,
                                double *pos, double *vel)
{
   double
        am, aovr, axnm, aynm, beta, beta2m, cape,
        cose, cosos, cs2f2g, csf, csfg, cslamb, di,
        diwc, dr, ecosf, fm, g1, g10, g13, g14, g2,
        g3, g4, g5, pm, r1, rdot, rm, rr, rvdot, sine,
        sini2, sinos, sn2f2g, snf, snfg, sni2du,
        snlamb, temp, ux, uy, uz, vx, vy, vz, xlamb,
        xmam, xmamdf, y4, y5, z1, z7, zc2, zc5;
  int i;

  /* Update for secular gravity and atmospheric drag */
  z1 = xndt*.5*tsince*tsince;
  z7 = two_thirds*3.5*z1/deep_arg->xnodp;
  xmamdf = tle->xmo+deep_arg->xmdot*tsince;
  deep_arg->omgadf = tle->omegao+deep_arg->omgdot*tsince+z7*xgdt1;
  deep_arg->xnode = tle->xnodeo+deep_arg->xnodot*tsince+z7*xhdt1;
  deep_arg->xn = deep_arg->xnodp;

  /* Update for deep-space secular effects */
  deep_arg->xll = xmamdf;
  deep_arg->t = tsince;
  Deep_dpsec( tle, deep_arg);
  xmamdf = deep_arg->xll;
  deep_arg->xn += xndt*tsince;
  deep_arg->em += edot*tsince;
  xmam = xmamdf+z1+z7*xmdt1;

  /* Update for deep-space periodic effects */
  deep_arg->xll = xmam;
  Deep_dpper( deep_arg);
  xmam = deep_arg->xll;
  xmam = FMod2p(xmam);

  /* Solve Kepler's equation */
  zc2 = xmam+deep_arg->em*sin(xmam)*(deep_arg->em*cos(xmam)+1.);

  i = 0;
  do
    {
      sine = sin(zc2);
      cose = cos(zc2);
      zc5 = 1./(1.-deep_arg->em*cose);
      cape = (xmam+deep_arg->em*sine-zc2)*zc5+zc2;
      r1 = cape-zc2;
      if (fabs(r1) <= e6a) break;
      zc2 = cape;
    }
  while(i++ < 10);

  /* Short period preliminary quantities */
  am = pow( xke / deep_arg->xn, two_thirds);
  beta2m = 1.f-deep_arg->em*deep_arg->em;
  sinos = sin(deep_arg->omgadf);
  cosos = cos(deep_arg->omgadf);
  axnm = deep_arg->em*cosos;
  aynm = deep_arg->em*sinos;
  pm = am*beta2m;
  g1 = 1./pm;
  g2 = ck2*.5*g1;
  g3 = g2*g1;
  beta = sqrt(beta2m);
  g4 = a3cof*.25*deep_arg->sinio;
  g5 = a3cof*.25*g1;
  snf = beta*sine*zc5;
  csf = (cose-deep_arg->em)*zc5;
  fm = atan2(snf, csf);
  if( fm < 0.)
     fm += pi + pi;
  snfg = snf*cosos+csf*sinos;
  csfg = csf*cosos-snf*sinos;
  sn2f2g = snfg*2.*csfg;
  r1 = csfg;
  cs2f2g = r1*r1*2.-1.;
  ecosf = deep_arg->em*csf;
  g10 = fm-xmam+deep_arg->em*snf;
  rm = pm/(ecosf+1.);
  aovr = am/rm;
  g13 = deep_arg->xn*aovr;
  g14 = -g13*aovr;
  dr = g2*(unmth2*cs2f2g-tthmun*3.)-g4*snfg;
  diwc = g3*3.*deep_arg->sinio*cs2f2g-g5*aynm;
  di = diwc*deep_arg->cosio;
  sini2 = sin(deep_arg->xinc*.5);

  /* Update for short period periodics */
  sni2du = sinio2*(g3*((1.-deep_arg->theta2*7.)*.5*sn2f2g-unm5th*
      3.*g10)-g5*deep_arg->sinio*csfg*(ecosf+2.))-g5*.5*
           deep_arg->theta2*axnm/cosio2;
  xlamb = fm+deep_arg->omgadf+deep_arg->xnode+g3*((deep_arg->cosio*6.+
     1.-deep_arg->theta2*7.)*.5*sn2f2g-(unm5th+deep_arg->cosio*2.)*
     3.*g10)+g5*deep_arg->sinio*(deep_arg->cosio*axnm/
     (deep_arg->cosio+1.)-(ecosf+2.)*csfg);
  y4 = sini2*snfg+csfg*sni2du+snfg*.5*cosio2*di;
  y5 = sini2*csfg-snfg*sni2du+csfg*.5*cosio2*di;
  rr = rm+dr;
  rdot = deep_arg->xn*am*deep_arg->em*snf/beta+g14*(g2*2.*unmth2*sn2f2g+g4*csfg);
  r1 = am;
  rvdot = deep_arg->xn*(r1*r1)*beta/rm+g14*dr+am*g13*deep_arg->sinio*diwc;

  /* Orientation vectors */
  snlamb = sin(xlamb);
  cslamb = cos(xlamb);
  temp = (y5*snlamb-y4*cslamb)*2.;
  ux = y4*temp+cslamb;
  vx = y5*temp-snlamb;
  temp = (y5*cslamb+y4*snlamb)*2.;
  uy = -y4*temp+snlamb;
  vy = -y5*temp+cslamb;
  temp = sqrt(1.-y4*y4-y5*y5)*2.;
  uz = y4*temp;
  vz = y5*temp;

  /* Position and velocity */
  pos[0] = rr*ux*xkmper;
  pos[1] = rr*uy*xkmper;
  pos[2] = rr*uz*xkmper;
  if( vel)
     {
     vel[0] = (rdot*ux+rvdot*vx)*xkmper;
     vel[1] = (rdot*uy+rvdot*vy)*xkmper;
     vel[2] = (rdot*uz+rvdot*vz)*xkmper;
     }

} /* SDP8 */