OrbMnvrHohmann:

Path: Orbit/OrbitManeuver

% Computes the delta-V for a Hohmann transfer between circular orbits. 
 The delta-Vs are at:

  1. The initial orbit
  2. The final orbit

 Type OrbMnvrHohmann for a demo with a plot.
--------------------------------------------------------------------------
   Form:
   [deltaV, tOF] = OrbMnvrHohmann( rI, rF, mu )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   rI          (1,1)  Initial 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
   tOF         (1,1)  Time of flight

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

Children:

Orbit: OrbitCoord/SLR
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/CP2I
SC: BasicOrbit/E2M
SC: BasicOrbit/E2Nu
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: BasicOrbit/Period
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/TitleS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Math: Linear/DupVect

Back to the Orbit Module page