Path: Orbit/OrbitMechanics
% Monte-Carlo orbit simulation. Type RandomOrbit for a demo with 2008 AE9 Since version 11. -------------------------------------------------------------------------- Form: [r1S, v1S, rN, vN] = RandomOrbit( el, el1S, t, mu, n ) -------------------------------------------------------------------------- ------ Inputs ------ elI (1,6) Elements vector [a,i,W,w,e,M] el1S (1,6) Gaussian noise vector [a,i,W,w,e,M] t (1,1) Times from 0 to ƒ (sec) mu (1,1) Gravitational parameter ------- Outputs ------- r1S (3,1) Mean position 1 sigma (km) v1S (3,1) Mean velocity 1 sigma (km) rN (3,1) Nominal position (km) vN (3,1) Nominal velocity (km) --------------------------------------------------------------------------
Common: Database/Constant Math: Linear/Mag Orbit: OrbitMechanics/RVOrbGen
Back to the Orbit Module page