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Robust Model Following Control Design for Missile Roll Autopilot

Gezer, R. Berk
Kutay, Ali Türker
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.