Path: FormationFlying/SafeGuidance
% Compute a delta-v that will change the current relative trajectory to a
2x1 ellipse centered about the TARGET. The delta-v should be applied at
the same time that corresponds to the supplied state.
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Form:
dV = EllipseDeltaV( r0, v0, n, x0 );
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Inputs
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r0 (6,1) Initial SLO-frame relative position [km]
v0 (6,1) Initial SLO-frame relative velocity [km/s]
n (1) Mean orbit rate (rad/s)
x0 (1) Desired along-track offset of ellipse [km]
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Outputs
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dV (3,1) SLO-frame delta-v [km/s]
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FormationFlying: SafeGuidance/HillsEqnsSLO
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