L1 Adaptive Controller for a Missile Longitudinal Autopilot Design
نویسندگان
چکیده
This paper considers application of L1 adaptive output feedback controller to a missile longitudinal autopilot design. The proposed adaptive controller has satisfactory performance in the presence of parametric uncertainties and time-varying disturbances. Simulations demonstrate the benefits of the control method and compare the results to Linear Quadratic Regulator (LQR) and Linear Quadratic Gaussian (LQG) with Loop Transfer Recovery (LTR) design.
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