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SUPPORT SITE |
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Path: Orbit/OrbitControl
% Converts the transfer time to delta-V for a rendezvous.
Uses the MATLAB function fmins to optimize the start and transfer times
for the maneuver. Draws a figure for no outputs.
See also LambertOpt.
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Forms:
maneuver = TransferTimeToDV( elT, elC, transferTime, mu, tol, planet )
maneuver = TransferTimeToDV
TransferTimeToDV
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Inputs
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elT (6,1) Target orbit elements for current position
elC (6,1) Chase orbit elements for current position
transferTime (1,2) Transfer times [nominal max]
mu (1,1) Gravitational parameter*
tol (1,1) Tolerance*
planet (:) Orbit center*
* Optional
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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
.u (3,2) Unit vectors of thrust
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Common: Graphics/Map Common: Graphics/NewFig Common: Graphics/TitleS Orbit: OrbitControl/LambertOpt Orbit: OrbitMechanics/RVOrbGen Orbit: OrbitMechanics/THohmn SC: BasicOrbit/El2RV
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