AE 168 - Aerospace Vehicle Dynamics and Control

3 units
Aircraft/spacecraft dynamics, stability and control. Linearization and Euler transformations. Eigenvalues and eigenvectors. State space and transfer function analysis of dynamics of aerospace vehicles. Feedback control design and synthesis using advanced control techniques.

Prerequisite(s): AE 140, AE 157, AE 165 and MATH 129A with a grade of ‘C-’ or better in each. Allowed Declared Majors: Aerospace Engineering. or Graduate Standing
Grading: Graded

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