Path: Orbit/Optimization
% Propagate and plot a 3D trajectory using costate outputs from optimization.
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Form:
b = Plot3DTrajectory( lambda, d, units, plotTitle )
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Inputs
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lambda (6,1) Costates
d (1,1) Structure to pass to fun
.costFun
.mu
.rF
.xF
.el0 (1,6) Initial orbit orbital elements
.elF (1,6) Final orbit orbital elements
units (1,:) Units for position
plotTitle (1,:) Title for plots
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Outputs
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b (1,1) Data structure
.r (3,:) Position
.v (3,:) Velocity
.t (1,:) Times
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SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler Sail: Coordinates/MEQToECI Sail: Coordinates/MEqToEl Sail: Coordinates/MEqToRV Common: Database/Constant Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
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