FOrbLTE:

Path: Orbit/RHSOrbit

% Orbit model for low thrust escapes.
   Designed for use with ode113. Includes a state for the mass and for the
   total delta-V, obtained by integrating the applied acceleration. Thrust
   and uE are treated as constant.
   See also LowThrustSim.
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   Form:
   vargout = FOrbLTE( t, x, flag, d )
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   ------
   Inputs
   ------
   t                      Time
   x             (n,1)    The state vector [r;v;m;DV]
   flag          (1,:)    Flags for ode113
   d             (1,1)    Data structure
                          .thrust  Engine thrust (N)
                          .mu      Gravitational parameter
                          .uE      Exhuast velocity (m/s)

   -------
   Outputs
   -------
   xDot          (n,1)     The state vector derivative d[r1;v1;r2;v2...]/dt

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Children:

Math: Linear/Mag
Math: Linear/Unit

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