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.

Lecture 2 hours/Lab 3 hours.

Prerequisite(s): C or better in AE 140, AE 157, and AE 165, or graduate standing.
Grading: Letter Graded

Class Schedule | Syllabus Information | Spartan Bookstore