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Sep 01, 2024
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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
Class Schedule | Syllabus Information | University Bookstore
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