Path: Missions/AsteroidProspector
% Simulation of low thrust maneuver to rendezvous with target orbit.
Applies constant magnitude, variable direction thrust to optimally
change each element one at a time, according to specified order.
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Form:
[t,el,r,v,mass,acc,accRSW] = LowThrustRendezvousSim( ...
el0, elT, mass0, thrust, Isp, elemOrder, mu);
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Inputs
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el0 (1,6) Initial Keplerian orbital elements [a,i,W,w,e,M]
elT (1,6) Target Keplerian orbital elements
mass0 (1,1) Initial mass (kg)
thrust (1,1) Thrust magnitude (kN)
Isp (1,1) Specific impulse (s)
elemOrder (1,5) Order in which to change elements
mu (1,1) Gravitational constant
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Outputs
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t (1,:) Simulation time vector
el (:,6) Orbital elements
r (3,:) Inertial position
v (3,:) Inertial velocity
mass (1,:) Mass
acc (3,:) Accleration in inertial frame
accRSW (3,:) Acceleration in RSW (radial / tangent / normal)
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See also: LowThrustTimeToTransfer, LowThrustGVE_EventFcn, LowThrustGVERHS
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AC: ACData/ACTConstants Missions: AsteroidProspector/GVEGuidance Missions: AsteroidProspector/LowThrustGVERHS Missions: AsteroidProspector/LowThrustGVE_EventFcn 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: BasicOrbit/Period SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: GUIs/ODETimeDisplay 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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