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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Orbit: OrbitControl/LambertOpt Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/LambertTOF Orbit: OrbitMechanics/PAHohmn Orbit: OrbitMechanics/RVOrbGen Orbit: OrbitMechanics/SynPer Orbit: OrbitMechanics/THohmn Orbit: OrbitMechanics/TTrnsHoh Orbit: OrbitMechanics/TWaitHoh 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 Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/DispWithTitle Common: General/IsVersionAfter Common: General/MatToCell Common: General/StringToTokens Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Ellipsd Common: Graphics/Map 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: Integration/RK45 Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
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