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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/Dynamics
% AKM Burn right-hand-side Since version 1. -------------------------------------------------------------------------- Form: xDot = FAKM( x, t, inr, inrDot, mRDot, hMWA, inrDamper, cDamper, uDamper, tAKM, tBurn ) -------------------------------------------------------------------------- ------ Inputs ------ x (8,1) The state vector t (1,1) Time inr (3,3) Inertia inrDot (3,3) Inertia derivative mRDot (3,3) Jet damping term hMWA (3,1) Wheel momentum vector inrDamper (1,1) Damper wheel inertia cDamper (1,1) Damper damping coefficient uDamper (3,1) Damper unit vector tAKM (3,1) AKM torque tBurn (1,1) Burn duration ------- Outputs ------- xDot (8,1) The derivative of the state state vector --------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot Math: Linear/Cross
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