Path: Orbit/OrbitManeuver

% Computes the delta-V to insert into a planetary or lunar orbit.
 The maneuver is done instantaneously. The default mu is for the
 Earth's moon.

 Type OrbMnvrInsertion for a lunar insertion demo.
    deltaV = OrbMnvrInsertion( r, v, rT, vT, rP, i, mu, qCToP )

   r           (3,1)  Spacecraft position in central body frame
   v           (3,1)  Spacecraft velocity in the central body frame
   rT          (3,1)  Planet position in the central body frame
   vT          (3,1)  Planet velocity in the central body frame
   rP          (1,1)  Perigee altitude (km)
   i           (1,1)  Planet orbit inclination (rad)
   mu          (1,1)  Gravitational parameter (Moon is the default)
   qCToP       (4,1)  Quaternion from central body to planet fixed frame

   deltaV      (3,1)  Vector velocity change in the central body frame



AC: ACData/ACTConstants
Orbit: OrbitCoord/RPRA2AE
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
SC: BasicOrbit/RV2El
SC: BasicOrbit/RVFromKepler
SC: BasicOrbit/VOrbit
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
Common: Graphics/Mesh2
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/Plot3D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Quaternion/QForm
Math: Linear/Cross
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit

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