LTVCon:

Path: Orbit/OrbitManeuver

% Solve the Linear Terminal Velocity Constraint problem.
   dr/dt = c1 + c2*vH where vH is the horizontal velocity and c1
   and c2 are constants

   Since version 2.
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   Form:
   v0 = LTVCon( r0, r, c1, c2, orbitType, mu )
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   ------
   Inputs
   ------
   r0            (3,1)   Initial position vector
   r             (3,1)   Final position vector
   c1            (1,1)   Constant
   c2            (1,1)   Constant
   orbitType     (1,:)   'direct' or 'retrograde'
   mu            (1,1)   Gravitational parameter (default is the earth)

   -------
   Outputs
   -------
   v0            (1,1)    Initial velocity

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	References:	Bond, V.R. and M. C. Allman, "Modern Astrodynamics", Princeton
             University Press, 1996, pp. 88-90
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Children:

Math: Linear/Mag
Orbit: OrbitMechanics/TARes

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