RHSTSTO:

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   Compute position, velocity and mass derivatives for a launch vehicle.
   The model assumes a rotating spherical planet.
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   Form:
   xDot = RHSTSTO( x, t, d )
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   ------
   Inputs
   ------
   x           (14,1)  [r v m r v m]
   t           (1,1)  Time (not used)
   d           (1,1)  Data structure
                      .rPlanet     (1,1) Planet radius (km)
                      .omega       (1,1) Planet rate (rad/s)
                      .mu          (1,1) Gravitational parameter
                      .vehicle1    (1,1) Vehicle 1 data structure
                      .vehicle2    (1,1) Vehicle 1 data structure

   -------
   Outputs
   -------
   xDot        (14,1)  Stage structural ratios

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Children:

Propulsion: LVModels/LiftingReentry3D