SeparationGuidance:

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   The Separation Guidance method.
   Maneuver immediately to separate spacecraft and exit avoidance region.

 Desired relative velocity along in-plane projection of pos. vector
  Direction is AWAY from TARGET, with minimum along-track component
  Magnitude is inversely proportional to distance from ellipse

 Correction made to along-track component to ensure sufficient drift such
  that the avoidance region is not reentered.

   Since version 10.
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   Form:
   deltaV = SeparationGuidance( parameters, state );
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   Inputs
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   parameters    (.)    Parameters that may be adjusted
   state         (.)    Absolute and relative state information

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   Outputs
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   deltaV        (.)    Delta-V sequence data structure
                          .dV  (3,N) Set of N Hills-frame delta-v's [km/s]
                          .t   (1,N) Time for each delta-v's [MET]

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Children:

FormationFlying: SafeGuidance/AlongTrackMotion