RHSTSTO:

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   Compute state and mass derivatives for a two-stage launch vehicle.
   The model assumes a rotating spherical planet.
  
   Since version 1.0
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   Form:
   xDot = RHSTSTO( x, t, d )
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   ------
   Inputs
   ------
   x          (14,1)  [r v m r v m] states of the two stages
   t           (1,1)  Time (not used)
   d            (.)   Data structure
                      .rPlanet     (1,1) Planet radius (km)
                      .omega       (1,1) Planet rate (rad/s)
                      .mu          (1,1) Gravitational parameter
                      .vehicle1     (.)  Vehicle 1 data structure
                      .vehicle2     (.)  Vehicle 2 data structure

   -------
   Outputs
   -------
   xDot        (14,1)  Derivatives

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   See also RHSLiftingReentry3D
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Children:

LaunchVehicle: LVModels/RHSLiftingReentry3D