AE 157 - Aerospace Automatic Control Systems Design

3 units
Modeling and analysis of aerospace feedback control systems. Stability analysis, root locus design, and frequency response methods for aerospace vehicles and associated automatic control systems. Nyquist/Bode diagrams. Lead-lag, PID compensator designs for aircraft and spacecraft.

Prerequisite(s): MATH 129A, MATH 133A, AE 138 w. a grade of “C-” or better in each. Or Graduate Standing
Grading: Graded

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