TriangularManeuver:

Path: Orbit/OrbitManeuver

% Compute maneuver profile for a triangular maneuver.
 r is the perpendicular bisector. The triangle is assumed to be
 equilateral. This maneuvers in a triangle around a point. This
 is useful for maneuvering around a target.
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   Form:
   [dV, fuel] = TriangularManeuver( p, r, m, t, uE )
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   ------
   Inputs
   ------
   p            (1,1)     Period (min)
   r            (1,1)     Perpendicular bisector of maneuver (m)
   m            (1,1)     Mass (kg)
   t            (1,1)     Duration (min)
   uE           (1,1)     Exhaust velocity (m/sec)

   -------
   Outputs
   -------
   dV           (1,1)     Total delta-V (m/s)
   fuel         (1,1)     Fuel consumption (kg)

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Children:

Math: Trigonometry/TanD

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