OptDIH:

Path: Orbit/OrbitManeuver

% Optimal inclination corrections for a Hohmann transfer with a plane change. 
 The Hohman transfer is done from the perigee of the first orbit to the 
 apogee of the second.
--------------------------------------------------------------------------
   Form:
   [dv, dv1, dv2, et, Di1] = OptDIH( e1, a1, e2, a2, Di, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   e1                    Parking orbit eccentricity 
   a1                    Parking orbit semimajor axis 
   e2                    Final orbit eccentricity 
   a2                    Final orbit semimajor axis 
   Di                    Change in inclination (rad)
   mu                    Gravitational parameter 

   -------
   Outputs
   -------
   dv                    Total delta v
   dv1                   Low orbit to transfer orbit delta v
   dv2                   Transfer orbit to high orbit delta v
   et                    Transfer orbit eccentricity
   Di1                   Inclination correction during first Dv

--------------------------------------------------------------------------
	References:	Hornbeck, R., Numerical Methods, Quantum, 1975, pp. 66-67.
--------------------------------------------------------------------------

Children:

Orbit: OrbitCoord/A2Apogee
Orbit: OrbitCoord/A2Perige
Common: General/DeBlankLT
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/PltStyle
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Math: Linear/DupVect

Back to the Orbit Module page