Path: Orbit/OrbitMechanics
% Computes the wait time at the target.
Since version 1.
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Form:
T = TWaitHoh( R1, R2, mu )
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Inputs
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R1 Orbit radius 1
R2 Orbit radius 2
mu Gravitational parameter
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Outputs
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T Wait time (sec)
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References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988,
pp. 294.
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Orbit: OrbitMechanics/SynPer Orbit: OrbitMechanics/TTrnsHoh
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