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): Grade of “C” or better in MATH 33A, MATH 39, AE 138 or Graduate Standing.
Grading: Graded

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