OrbMnvrInclAndHohm:

Path: Orbit/OrbitManeuver

% Delta-V for a Hohmann transfer between circular non coplanar orbits.
   The delta-Vs are at

     The initial orbit
     The final orbit

--------------------------------------------------------------------------
   Form:
   [deltaV, deltaI, tOF] = OrbMnvrInclAndHohm( rI, rF, iI, iF, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   rI          (1,1)  Initial radius
   rF          (1,1)  Final radius
   II          (1,1)  Initial inclination (rad)
   iF          (1,1)  Final inclination (rad)
   mu          (1,1)  Gravitational parameter

   -------
   Outputs
   -------
   deltaV      (1,1)  Delta-V data structure. 
                      .total (1,1)	Total required delta-V
                      .a     (1,1) Delta-V at point a
                      .b     (1,1) Delta-V at point b
   deltaI      (1,1)  Delta-Inclination data structure. 
                      .total (1,1)	Total required delta-V (rad)
                      .a     (1,1) Delta-Inclination at point a (rad)
                      .b     (1,1) Delta-Inclination at point b (rad)
   tOF         (1,1)  Time of flight

--------------------------------------------------------------------------
   Reference: Vallado, D. A. (1997.) Fundamentals of Astrodynamics and
              Applications. pp 281-282.
--------------------------------------------------------------------------

Back to the Orbit Module page