AstroToolbox/Astro_Functions.h

   1 // ------------------------------------------------------------------------ //
   2 // This source file is part of the 'ESA Advanced Concepts Team's                        //
   3 // Space Mechanics Toolbox' software.                                       //
   4 //                                                                          //
   5 // The source files are for research use only,                              //
   6 // and are distributed WITHOUT ANY WARRANTY. Use them on your own risk.     //
   7 //                                                                          //
   8 // Copyright (c) 2004-2007 European Space Agency                            //
   9 // ------------------------------------------------------------------------ //
  10
  11 #ifndef ASTRO_FUNCTIONS_H
  12 #define ASTRO_FUNCTIONS_H
  13
  14 // Conversion from Mean Anomaly to Eccentric Anomaly via Kepler's equation
  15 double Mean2Eccentric (const double &, const double &);
  16
  17 void Conversion(const double*, double*, double*, const double &);
  18
  19 double norm(const double*, const double*);
  20
  21 double norm2(const double*);
  22
  23 void vett(const double*, const double*, double*);
  24
  25 double tofabn(const double&, const double&, const double&);
  26
  27 void vers(const double*, double*);
  28
  29 double x2tof(const double&, const double&, const double&, const int &);
  30
  31 #endif
  32
  33
  34