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SUPPORT SITE |
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Path: Orbit/Interplanetary
% Transformation matrix from the heliocentric to B-plane frame. The B-plane frame is a plane moving with the planet and perpendicular to the incoming velocity of the asteroid. Type HelioToBPlane for a demo. Since version 2014.1 -------------------------------------------------------------------------- Form: [m, bN] = HelioToBPlane( r0, v0, rA, vA ) -------------------------------------------------------------------------- ------ Inputs ------ r0 (3,1) Position vector planet v0 (3,1) Velocity vector planet rA (3,1) Position vector asteroid vA (3,1) Velocity vector asteroid ------- Outputs ------- m (3,3) Transformation matrix n (3,1) Trajectory orbit normal bN (3,1) B-plane normal --------------------------------------------------------------------------
Common: Database/Constant Math: Linear/Cross Math: Linear/Dot Math: Linear/Unit Orbit: Interplanetary/PlotBPlane
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