Path: Orbit/OrbitManeuver
% Computes the transfer and phase angle given transfer time.
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Form:
[transferAngle, phaseAngle] = TransferAndPhaseAngle( r1, r2, tT, mu )
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Inputs
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r1 Orbit radius 1
r2 Orbit radius 2
tT TransferTime
mu Gravitational parameter
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Outputs
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transferAngle Transfer angle (rad)
phaseAngle Phase angle (rad)
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References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988,
pp. 292.
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