RendezvousPlanner:

Path: Orbit/OrbitControl

% Compute delta-Vs for rendezvous. 
 The inputs are the initial target position and velocity vector, the initial chase
 vehicle position and velocity vector, the time allowed for the rendezvous,
 the gravitational parameter and the tolerance for the Lambert problem 
 solver. It computes both direct and retrograde trajectories.
--------------------------------------------------------------------------
   Form:
   [dV1D, dV2D, dV1R, dV2R] = RendezvousPlanner( rT, vT, rC, vC, dT, planet, mu, tol )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   rT            (3,1)   Target orbit position
   vT            (3,1)   Target orbit velocity
   rC            (3,1)   Chase vehicle orbit position
   vC            (3,1)   Chase vehicle orbit velocity
   dT            (1,1)   Time between position 2 and 1
   planet        (1,1)   Name of planet
   mu            (1,1)   Gravitational parameter
   tol           (1,1)   Tolerance

   -------
   Outputs
   -------
   dV1D          (3,1)    Initial delta-V direct transfer
   dV2D          (3,1)    Final delta-V direct transfer
   dV1R          (3,1)    Initial delta-V retrograde transfer
   dV2R          (3,1)    Final delta-V retrograde transfer

--------------------------------------------------------------------------
   See also LambertTOF
--------------------------------------------------------------------------

Children:

Common: Graphics/Map
Common: Graphics/NewFig
Math: Linear/Mag
Orbit: OrbitMechanics/LambertTOF
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/El2RV
SC: BasicOrbit/RV2El

Back to the Orbit Module page