Path: Missions/AsteroidProspector
% Compute delta-v assuming full thrust applied during all transfer times.
Approximate delta-V required to transfer to another orbit. Assumes one
Keplerian element is changed at a time. Takes in transfer times from
another function.
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Form:
[dVTot,dVElem] = LowThrustDVToTransfer( dT, m0, thrust, Isp )
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Inputs
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dT (5,1) Transfer times for each orbital element (sec)
See LowThrustTimeToTransfer.m
m0 (1,1) Initial mass of spacecraft (kg)
thrust (1,1) Thrust magnitude (kN)
Isp (1,1) Specific impulse (sec)
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Outputs
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dVTot (1,1) Total delta-v for changing all elements (km/s)
dVElem (5,1) Delta-v for changing each element (km/s)
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AC: ACData/ACTConstants Missions: AsteroidProspector/GVEGuidance Missions: AsteroidProspector/LowThrustTimeToTransfer Orbit: OrbitCoord/OrbElemDiff Orbit: OrbitMechanics/GVEDynamics SC: BasicOrbit/CP2I 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: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Math: Linear/Cross Math: Linear/DupVect Math: Linear/Unit Math: Trigonometry/WrapPhase
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