Path: FormationFlying/Analysis
% Plot the trajectory that will result from a planned maneuver.
Given the current state & the maneuver planned using this state, plot the
trajectory throughout the maneuver and for an orbit after the final burn.
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Form:
[dElFinal,xHFinal] = CheckDeltaVs( state, maneuver, iD, nSPO, plotFlag );
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Inputs
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state (.) State data structure at time of maneuver planning
maneuver (.) Maneuver data structure, computed using IterativeImpulsiveManeuver
iD (1) Spacecraft ID to distinguish plots
(optional, default is 1)
nSPO (1) Number of simulation points per orbit
(optional, default is 250)
plotFlag (1) Flag -- create plots (1) or not (0)
(optional, default is 1)
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Outputs
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dElFinal (:,6) Orbital element differences
xHFinal (6,:) Hills frame position and velocity
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FormationFlying: Dynamics/HillsEqns FormationFlying: EccDynamics/FFEccIntConst FormationFlying: EccDynamics/FFEccLawdensEqns FormationFlying: EccDynamics/FFEccRMat FormationFlying: Transformation/DeltaElem2Hills FormationFlying: Transformation/Hills2DeltaElem FormationFlying: Utility/Nu2TimeDomain FormationFlying: Utility/NuDot FormationFlying: Utility/Time2NuDomain Orbit: OrbitCoord/El2Alfriend Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu 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/OrbRate SC: BasicOrbit/Period SC: BasicOrbit/RV2El Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/Cross Math: Linear/DupVect Math: Linear/Mag Math: Trigonometry/UnwrapPhase Math: Trigonometry/WrapPhase
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