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Feedback Control of Attitude using Quaternions
I have a quaternion state space model of an aircraft and I can apply moments in the body frame to control its attitude. So I ...
13 years 前 | 0 个回答 | 0
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state space model with constant term
If i linearize a nonlinear system model of the form dx/dt=f(x,u) so that it can be written in the form dx/dt=Ax+Bu+consta...
13 years 前 | 2 个回答 | 0
