/[PAMELA software]/YodaProfiler/inc/sgp4.h
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revision 1.1 by mocchiut, Fri Oct 20 11:39:34 2006 UTC revision 1.4 by mocchiut, Tue Feb 6 13:01:03 2007 UTC
# Line 3  Line 3 
3  //  //
4  #ifndef sgp4_h  #ifndef sgp4_h
5  #define sgp4_h  #define sgp4_h
6  #pragma once  
7    #if !defined(__CINT__) || defined(__MAKECINT__)
8    
9  //#define WIN32_LEAN_AND_MEAN   // Exclude rarely-used stuff from Windows headers  //#define WIN32_LEAN_AND_MEAN   // Exclude rarely-used stuff from Windows headers
10  #include <stdio.h>  #include <stdio.h>
11  //#include <tchar.h>  //#include <tchar.h>
12    #include <ctype.h>
13  #include <string>  #include <string>
14  #include <map>  #include <map>
15  #include <vector>  #include <vector>
# Line 378  protected: Line 379  protected:
379     cJulian  m_date;     cJulian  m_date;
380     VecUnits m_VecUnits;     VecUnits m_VecUnits;
381  };  };
382    //
383    // cNoradBase.h
384    //
385    // This class provides a base class for the NORAD SGP4/SDP4
386    // orbit models.
387    //
388    // Copyright (c) 2003 Michael F. Henry
389    //
390    #pragma once
391    
392    //////////////////////////////////////////////////////////////////////////////
393    
394    class cEci;
395    class cOrbit;
396    
397    //////////////////////////////////////////////////////////////////////////////
398    
399    class cNoradBase
400    {
401    public:
402       cNoradBase(const cOrbit&);
403       virtual ~cNoradBase() {};
404    
405       virtual bool getPosition(double tsince, cEci &eci) = 0;
406    
407    protected:
408       cNoradBase& operator=(const cNoradBase&);
409    
410       void Initialize();
411       bool FinalPosition(double  incl, double omega,  double     e,  
412                          double     a, double    xl,  double xnode,
413                          double    xn, double tsince, cEci &eci);
414    
415       const cOrbit &m_Orbit;
416    
417       // Orbital parameter variables which need only be calculated one
418       // time for a given orbit (ECI position time-independent).
419       double m_satInc;  // inclination
420       double m_satEcc;  // eccentricity
421    
422       double m_cosio;   double m_theta2;  double m_x3thm1;  double m_eosq;  
423       double m_betao2;  double m_betao;   double m_aodp;    double m_xnodp;
424       double m_s4;      double m_qoms24;  double m_perigee; double m_tsi;
425       double m_eta;     double m_etasq;   double m_eeta;    double m_coef;
426       double m_coef1;   double m_c1;      double m_c2;      double m_c3;
427       double m_c4;      double m_sinio;   double m_a3ovk2;  double m_x1mth2;
428       double m_xmdot;   double m_omgdot;  double m_xhdot1;  double m_xnodot;
429       double m_xnodcf;  double m_t2cof;   double m_xlcof;   double m_aycof;
430       double m_x7thm1;
431    };
432    //
433    // cOrbit.h
434    //
435    // This is the header file for the class cOrbit. This class accepts a
436    // single satellite's NORAD two-line element set and provides information
437    // regarding the satellite's orbit such as period, axis length,
438    // ECI coordinates/velocity, etc., using the SGP4/SDP4 orbital models.
439    //
440    // Copyright (c) 2002-2003 Michael F. Henry
441    //
442    #pragma once
443    
444    #include "math.h"
445    
446    using namespace std;
447    //////////////////////////////////////////////////////////////////////////////
448    
449    class cVector;
450    class cGeoCoord;
451    class cEci;
452    
453    //////////////////////////////////////////////////////////////////////////////
454    class cOrbit  
455    {
456    public:
457       cOrbit(const cTle &tle);
458       virtual ~cOrbit();
459    
460       // Return satellite ECI data at given minutes since element's epoch.
461       bool getPosition(double tsince, cEci *pEci) const;
462      
463       double Inclination()  const { return radGet(cTle::FLD_I);                 }
464       double Eccentricity() const { return m_tle.getField(cTle::FLD_E);         }
465       double RAAN()         const { return radGet(cTle::FLD_RAAN);              }
466       double ArgPerigee()   const { return radGet(cTle::FLD_ARGPER);            }
467       double BStar()        const { return m_tle.getField(cTle::FLD_BSTAR) / AE;}
468       double Drag()         const { return m_tle.getField(cTle::FLD_MMOTIONDT); }
469       double mnMotion()     const { return m_tle.getField(cTle::FLD_MMOTION);   }
470       double mnAnomaly()    const { return radGet(cTle::FLD_M);                 }
471       double mnAnomaly(cJulian t) const;  // mean anomaly (in radians) at time t
472    
473       cJulian Epoch() const { return m_jdEpoch; }
474    
475       double TPlusEpoch(const cJulian &t) const;    // time span [t - epoch] in secs
476    
477       string SatName(bool fAppendId = false) const;
478      
479       // "Recovered" from the input elements
480       double SemiMajor()   const { return m_aeAxisSemiMajorRec; }
481       double SemiMinor()   const { return m_aeAxisSemiMinorRec; }
482       double mnMotionRec() const { return m_mnMotionRec; }  // mn motion, rads/min
483       double Major()   const { return 2.0 * SemiMajor(); }  // major axis in AE
484       double Minor()   const { return 2.0 * SemiMinor(); }  // minor axis in AE
485       double Perigee() const { return m_kmPerigeeRec;    }  // perigee in km
486       double Apogee()  const { return m_kmApogeeRec;     }  // apogee in km
487       double Period()  const;                               // period in seconds
488    
489    protected:
490       double radGet(cTle::eField fld) const
491          { return m_tle.getField(fld, cTle::U_RAD); }
492    
493       double degGet(cTle::eField fld) const
494          { return m_tle.getField(fld, cTle::U_DEG); }
495    
496    private:
497       cTle        m_tle;
498       cJulian     m_jdEpoch;
499       cNoradBase *m_pNoradModel;
500    
501       // Caching variables; note units are not necessarily the same as tle units
502       mutable double m_secPeriod;
503    
504       // Caching variables recovered from the input TLE elements
505       double m_aeAxisSemiMinorRec;  // semi-minor axis, in AE units
506       double m_aeAxisSemiMajorRec;  // semi-major axis, in AE units
507       double m_mnMotionRec;         // radians per minute
508       double m_kmPerigeeRec;        // perigee, in km
509       double m_kmApogeeRec;         // apogee, in km
510    };
511    
512    //
513    // cNoradSGP4.h
514    //
515    // This class implements the NORAD Simple General Perturbation 4 orbit
516    // model. This model provides the ECI coordiantes/velocity of satellites
517    // with orbit periods less than 225 minutes.
518    //
519    // Copyright (c) 2003 Michael F. Henry
520    //
521    #pragma once
522    
523    class cOrbit;
524    
525    //////////////////////////////////////////////////////////////////////////////
526    class cNoradSGP4 : public cNoradBase
527    {
528    public:
529       cNoradSGP4(const cOrbit &orbit);
530       virtual ~cNoradSGP4() {};
531    
532       virtual bool getPosition(double tsince, cEci &eci);
533    
534    protected:
535       double m_c5;
536       double m_omgcof;
537       double m_xmcof;
538       double m_delmo;
539       double m_sinmo;
540    };
541    
542    //
543    // cNoradSDP4.h
544    //
545    // This class implements the NORAD Simple Deep Perturbation 4 orbit
546    // model. This model provides the ECI coordinates/velocity of satellites
547    // with periods >= 225 minutes.
548    //
549    // Copyright (c) 2003 Michael F. Henry
550    //
551    #pragma once
552    
553    class cOrbit;
554    
555    //////////////////////////////////////////////////////////////////////////////
556    class cNoradSDP4 : public cNoradBase
557    {
558    public:
559       cNoradSDP4(const cOrbit &orbit);
560       virtual ~cNoradSDP4() {};
561    
562       virtual bool getPosition(double tsince, cEci &eci);
563    
564    protected:
565       bool DeepInit(double *eosq,    double *sinio,    double *cosio,  double *m_betao,
566                     double *m_aodp,  double *m_theta2, double *m_sing, double *m_cosg,
567                     double *m_betao2,double *xmdot,    double *omgdot, double *xnodott);
568    
569       bool DeepSecular(double *xmdf,  double *omgadf,double *xnode, double *emm,
570                        double *xincc, double *xnn,   double *tsince);
571       bool DeepCalcDotTerms  (double *pxndot, double *pxnddt, double *pxldot);
572       void DeepCalcIntegrator(double *pxndot, double *pxnddt, double *pxldot,
573                               const double &delt);
574       bool DeepPeriodics(double *e,     double *xincc,  double *omgadf,
575                          double *xnode, double *xmam);
576       double m_sing;
577       double m_cosg;
578    
579       // Deep Initialization
580       double eqsq;   double siniq;  double cosiq;  double rteqsq; double ao;  
581       double cosq2;  double sinomo; double cosomo; double bsq;    double xlldot;
582       double omgdt;  double xnodot;
583      
584       // Deep Secular, Periodic
585       double xll;    double omgasm; double xnodes; double _em;    
586       double xinc;   double xn;     double t;
587    
588       // Variables shared by "Deep" routines
589       double dp_e3;     double dp_ee2;    double dp_savtsn; double dp_se2;
590       double dp_se3;    double dp_sgh2;   double dp_sgh3;   double dp_sgh4;
591       double dp_sghs;   double dp_sh2;    double dp_sh3;    double dp_si2;
592       double dp_si3;    double dp_sl2;    double dp_sl3;    double dp_sl4;
593       double dp_xgh2;   double dp_xgh3;   double dp_xgh4;   double dp_xh2;
594       double dp_xh3;    double dp_xi2;    double dp_xi3;    double dp_xl2;
595       double dp_xl3;    double dp_xl4;    double dp_xqncl;  double dp_zmol;
596       double dp_zmos;
597    
598       double dp_atime;  double dp_d2201;  double dp_d2211;  double dp_d3210;
599       double dp_d3222;  double dp_d4410;  double dp_d4422;  double dp_d5220;
600       double dp_d5232;  double dp_d5421;  double dp_d5433;  double dp_del1;
601       double dp_del2;   double dp_del3;   double dp_fasx2;  double dp_fasx4;
602       double dp_fasx6;  double dp_omegaq; double dp_sse;    double dp_ssg;
603       double dp_ssh;    double dp_ssi;    double dp_ssl;    double dp_step2;
604       double dp_stepn;  double dp_stepp;  double dp_thgr;   double dp_xfact;
605       double dp_xlamo;  double dp_xli;    double dp_xni;
606    
607       bool dp_iresfl;
608       bool dp_isynfl;
609    
610       // DeepInit vars that change with epoch
611       double dpi_c;      double dpi_ctem;   double dpi_day;    double dpi_gam;
612       double dpi_stem;   double dpi_xnodce; double dpi_zcosgl; double dpi_zcoshl;
613       double dpi_zcosil; double dpi_zsingl; double dpi_zsinhl; double dpi_zsinil;
614       double dpi_zx;     double dpi_zy;
615    
616    };
617    
618  #endif  #endif
619    #endif
620    
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