OrbMnvrBielliptic:

Path: Orbit/OrbitManeuver

% Delta-V for a bielliptic orbit maneuver between circular orbits. 
   The intermediate radius is much larger than the final radius.
   The delta-Vs are at

   The initial orbit
   Apogee of the transfer orbit
   The final orbit

--------------------------------------------------------------------------
   Form:
   [deltaV, tOF] = OrbMnvrBielliptic( rI, rB, rF, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   rI          (1,1)  Initial radius
   rB          (1,1)  Intermediate radius
   rF          (1,1)  Final radius
   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
                      .c     (1,1) Delta-V at point c
   tOF         (1,1)  Time of flight

--------------------------------------------------------------------------

Back to the Orbit Module page