AE 157 - Aerospace Automatic Control Systems Design

3 unit(s)
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.

Lecture 2 hours/Lab 3 hours.

Prerequisite(s): “C” or better in MATH 33A, MATH 39, and AE 138 or graduate standing.
Grading: Letter Graded

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