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AERO 420. Aircraft Dynamics and Control. 4 units

Term Typically Offered: W

Prerequisite: AERO 306 and AERO 320.

Newton's 6-degree-of-freedom equations of motion applied to aerospace vehicles. Stability and control derivatives, reference frames, steady-state and perturbed dynamic analyses applied to aerospace vehicles. Stability and control design principles applied to transfer functions, state-space, and modal system dynamics. 4 lectures.

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...ENGR , FPE ) Aerospace Engineering ( AERO ) Biomedical Engineering ( BMED...Recommended: FSN 329 , FSN 420 and STAT 218...