BilinearTangentLaw:

Path: SCPro/Landers

% Bilinear tangent law for orbit insertion or landing.
   Assumes constant acceleration of gravity and constant engine
   accleration. For applicable landing or takeoff problems the first
   is true, the latter is usually not due to the decrease in mass of the
   vehicle. The thrust angle is from the horizontal and g is along 
   the vertical. It uses fminsearch to find the optimal angles.

   The launch or landing vector may not be vertical.

   Type BilinearTangentLaw for a demo from the reference.

   Units may be of any type as long as they are consistent.

   Since Version 11
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   Form:
   [beta, t] = BilinearTangentLaw( u, g, a, h, n, opt, dT )
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   ------
   Inputs
   ------
   u       (1,1)	Final or initial velocity
   g       (1,1)	Acceleration of gravity
   a       (1,1)	Engine acceleration
   h       (1,1)	Final or initial altitude
   n       (1,1)	Number of steps
   opt     (1,:)	fminsearch options
   dT      (1,1)	Time step in place of n

   -------
   Outputs
   -------
   beta    (1,n)	Thrust angle from horizontal
   t       (1,n)	Corresponding time vector
   tMin    (1,1) Minimum time

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   Reference: Arthur E. Bryson, Jr., Y. C. Ho, "Applied Optimal Control:
              Optimization, Estimation, and Control," Orbit, pp. 83-86.
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Children:

Common: Graphics/Plot2D

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