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 --------------------------------------------------------------------------