RE2SLO:
% Compute the SLO-frame state associated with a relative ellipse.
SLO = spacecraft local orbit, equivalent to LVLH frame
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Usage:
xSLO = RE2SLO( x, z, x0, aE, yA, yR, n );
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Inputs
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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]
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Outputs
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xSLO (1) SLO-frame state on relative ellipse
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