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 --------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: Interplanetary/PlotBPlane Orbit: OrbitMechanics/VEscape SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/MatToCell Common: General/Watermark Common: Graphics/Circle Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/Cross Math: Linear/Dot Math: Linear/Mag Math: Linear/Unit
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