Path: Orbit/OrbitManeuver

% Orbit separation demo
 Calculate a delta-V for an in-plane separation and size a thruster to perform
 the maneuver. This is a bang/bang maneuver.

 This demonstrates that a small satellite deployed in LEO can move 1 km away
 from the "mother ship" in less than one orbit with a range of thrusters. The
 Lambert delta-V approaches the ideal delta-V as the time approaches one orbit.


Orbit: OrbitControl/DVTarget
Orbit: OrbitManeuver/OrbMnvrPhaseChange
Orbit: OrbitMechanics/LambertTOF
SC: BasicOrbit/CP2I
SC: BasicOrbit/E2M
SC: BasicOrbit/E2Nu
SC: BasicOrbit/El2RV
SC: BasicOrbit/M2E
SC: BasicOrbit/M2EApp
SC: BasicOrbit/M2EEl
SC: BasicOrbit/M2EHy
SC: BasicOrbit/M2Nu
SC: BasicOrbit/M2NuPb
SC: BasicOrbit/Nu2E
SC: BasicOrbit/Nu2M
SC: BasicOrbit/RV2El
SC: BasicOrbit/RVFromKepler
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DispWithTitle
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/Plot3D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/TitleS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Math: Linear/Cross
Math: Linear/Dot
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit

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