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