Path: FormationFlying/SafeGuidance
% The Separation Guidance method.
Maneuver immediately to separate spacecraft and exit avoidance region.
Desired relative velocity along in-plane projection of pos. vector
Direction is AWAY from TARGET, with minimum along-track component
Magnitude is inversely proportional to distance from ellipse
Correction made to along-track component to ensure sufficient drift such
that the avoidance region is not reentered.
Since version 10.
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Form:
deltaV = SeparationGuidance( parameters, state );
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Inputs
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parameters (.) Parameters that may be adjusted
state (.) Absolute and relative state information
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Outputs
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deltaV (.) Delta-V sequence data structure
.dV (3,N) Set of N Hills-frame delta-v's [km/s]
.t (1,N) Time for each delta-v's [MET]
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FormationFlying: SafeGuidance/AlongTrackMotion FormationFlying: SafeGuidance/HillsEqnsSLO Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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