Path: FormationFlying/SafeGuidance
% Restrict the in-plane and cross-track components of the delta-v -------------------------------------------------------------------------- Form: dVSLO = RestrictDeltaV( dVSLO, xSLO, n, dMin, x0, aE ) -------------------------------------------------------------------------- ------ Inputs ------ dVSLO (3,1) Intended delta-v in SLO frame xSLO (6,1) Relative state, SLO-frame n (1) Mean orbit rate [rad/s] dMin (1) Min. separation distance [km] x0 (1) Desired along-track offset [km] aE (1) Desired Semi-major axis of relative ellipse [km] ------- Outputs ------- dVSLO (3,1) Restricted delta-v in SLO frame --------------------------------------------------------------------------
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