Applying mu -synthesis to missile autopilot design
- 1 January 1990
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 2993-2998 vol.6
- https://doi.org/10.1109/cdc.1990.203333
Abstract
mu -synthesis combines the structured singular value and H/sub infinity / 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.<>Keywords
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