Path: FormationFlying/SafeGuidance
% Compute the SLO-frame state associated with a relative ellipse. SLO is spacecraft local orbit, equivalent to LVLH frame ------------------------------------------------------------------------------- Form: xSLO = RE2SLO( x, z, x0, aE, yA, yR, n ); ------------------------------------------------------------------------------- ------ Inputs ------ x (1) Along-track position z (1) Radial position x0 (1) Center of along-track motion aE (1) Semi-major axis of relative ellipse yA (1) Cross-track offset at forward along-track axis crossing yR (1) Cross-track offset at high radial axis crossing n (1) Mean orbit rate [rad/s] ------- Outputs ------- xSLO (1) SLO-frame state on relative ellipse -------------------------------------------------------------------------------
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