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MECH 5101 [0.5 credit] (MCG 5311) Flight Dynamics and Automatic Flight Controls

Aircraft nonlinear equations of motion and their linearization; effect of stability and control derivatives on the open-loop dynamics response; autopilot design and aircraft stability and control augmentation; pilot-in-the-loop; aeroelastic effects on stability and control.
Includes: Experiential Learning Activity
Also listed as MAAJ 5151.