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SUPPORT SITE |
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Path: Orbit/OrbitManeuver
% Compute delta-Vs for rendezvous using Hohmann transfers.
The inputs are the target and chase spacecraft elements.
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Form:
maneuver = HohmannTransferRendezvous( elT, elC, mu, tol, planet )
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Inputs
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elT (6,1) Target orbit elements
elC (6,1) Chase orbit elements
mu (1,1) Gravitational parameter
tol (1,1) Tolerance
planet (1,:) Planet name
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Outputs
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maneuver (1,1) Maneuver data structure
.dV1 (1,1) Transfer orbit insertion delta-V
.dV2 (1,1) Target orbit insertion delta-V
.tStart (1,1) Start time relative to epoch
.tTransfer (1,1) Time in transfer orbit
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Common: Graphics/Map Common: Graphics/NewFig Math: Linear/Dot Math: Linear/Unit Orbit: OrbitManeuver/DVHoh Orbit: OrbitMechanics/LambertTOF Orbit: OrbitMechanics/RVOrbGen Orbit: OrbitMechanics/THohmn SC: BasicOrbit/El2RV SC: BasicOrbit/Period SC: BasicOrbit/RV2El
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