Robust Model Following Control Design for Missile Roll Autopilot

Date

2014-07-11

Author

Gezer, R. Berk
Kutay, Ali Türker

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This paper presents a robust model following control method augmented with error integration and Luenberger observer for anti-air missile roll autopilot designed using optimal control laws. The design is shown to be robust to external disturbance, noisy measurements and sensor lags by frequency domain analysis. The regulation performance of the controller is presented by simulations.

Subject Keywords

Model Following Control, Robust Control, Optimal Control, Missile Roll Autopilot

URI

https://hdl.handle.net/11511/55771

Conference Name

United-Kingdom-Automatic-Control-Council (UKACC) 10th International Conference on Control (CONTROL)

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

R. B. Gezer and A. T. Kutay, “Robust Model Following Control Design for Missile Roll Autopilot,” presented at the United-Kingdom-Automatic-Control-Council (UKACC) 10th International Conference on Control (CONTROL), Loughborough, UNITED KINGDOM, 2014, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/55771.