AA 212: Advanced Feedback Control Design

Aeronautics & Astronautics Stanford University 3.0 credits

Course Description

Analysis and design techniques for multivariable feedback systems. State-space concepts, observability, controllability, eigenvalues, eigenvectors, stability, and canonical representations. Approaches for robust feedback control design, chiefly H2, H-infinity, and mu-synthesis. System identification and adaptive control design. Use of computer-aided design with MATLAB. Prerequisite: ENGR 105. Recommended: Linear algebra (EE 263 or equivalent).

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