TransferAndPhaseAngle:

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
   ------
   r1                    Orbit radius 1
   r2                    Orbit radius 2
   tT                    TransferTime
   mu                    Gravitational parameter

   -------
   Outputs
   -------
   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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