Path: FormationFlying/Control
% Computes the delta-v's required for an in-plane maneuver.
Since version 7.
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Inputs
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meas_elem (1,6) Reference orbital elements (Alfriend format)
[a,theta,i,q1,q2,W]
delta_elem (:,6) Error in orbital element differences (Alfriend format)
accNom (1) Nominal acceleration [km/s/s]
dTMin (1) Minimum achievable burn duration [sec]
nOrbMin (1) Minimum number of orbits maneuver may last
nOrbMax (1) Maximum number of orbits maneuver may last
horizon (1) Minimum amount of time required prior to first burn [sec]
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Outputs
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burnData (.) Array of burn data structures with burn times,
durations, magnitudes and directions.
t0 (1) First burn time [sec from meas time]
tF (1) Final burn time [sec from meas time]
nBurns (1) Number of burns required
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AC: ACData/ACTConstants FormationFlying: Control/OptimalInPlaneDeltaV FormationFlying: Utility/TimeUntilTheta SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect Math: Trigonometry/WrapPhase
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