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SUPPORT SITE |
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Path: Orbit/OrbitManeuver
% Convert an acceleration vector into a thrust quaternion. Type AccelToThrustAndQ for a demo. -------------------------------------------------------------------------- Form: [thrust, q] = AccelToThrustAndQ( a, m, u ) -------------------------------------------------------------------------- ------ Inputs ------ a (3,:) Acceleration vector(s) m (1,1) Mass (kg) u (3,1) Thruster unit force vector in the body frame ------- Outputs ------- thrust (1,:) Thrust q (4,:) Quaternion --------------------------------------------------------------------------
Common: Graphics/Plot2D Common: Quaternion/QForm Common: Quaternion/U2Q Math: Linear/Mag Math: Linear/Unit
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