mu -synthesis combines the structured singular value and Hinfinity control to design compensators for plants with structured uncertainty. The application of mu -synthesis to the design of a flight control system for a highly maneuverable tail controlled missile is discussed. Performance goals are given in the time and frequency domains and include time constant, overshoot, stability margins, and high-frequency attenuation. The resulting control law desensitizes the system's performance to structured variations in the missile's aerodynamic properties and provides some robustness, in both a single-loop and a multiloop sense, to variations and/or perturbations not included in the uncertainty model.
Applying mu -synthesis to missile autopilot design
Autopilot für Flugkörper
Proceedings of the 29th IEEE Conference on Decision and Control ; 6 ; 2993-2998
1990
6 Seiten, 8 Quellen
Aufsatz (Konferenz)
Englisch
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