AE 168 - Aerospace Vehicle Dynamics and Control

3 unit(s)
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.

Lecture 2 hours/Lab 3 hours.

Prerequisite(s): “C” or better in AE 140, AE 157, AE 165 and MATH 39 or graduate standing. Allowed Declared Majors: Aerospace Engineering.
Grading: Letter Graded

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