Title :
Robust model following control design for missile roll autopilot
Author :
Berk Gezer, R. ; Kutay, Ali Turker
Author_Institution :
Eng. Dev. Directorate, Roketsan Missiles Inc., Ankara, Turkey
Abstract :
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.
Keywords :
attitude control; missile control; observers; optimal control; robust control; Luenberger observer; antiair missile roll autopilot; error integration; external disturbance; frequency domain analysis; noisy measurements; optimal control laws; regulation performance; robust model following control design; sensor lags; Aerodynamics; Frequency control; Missiles; Noise; Observers; Robustness; Transfer functions; Missile roll autopilot; Model following control; Optimal control; Robust control;
Conference_Titel :
Control (CONTROL), 2014 UKACC International Conference on
Conference_Location :
Loughborough
DOI :
10.1109/CONTROL.2014.6915107