Title :
Robust control design of an autolanding system
Author :
Ben Ghalia, Mounir ; Alouani, Ali T.
Author_Institution :
Tennessee Technol. Univ., Cookeville, TN, USA
Abstract :
A linear-quadratic-Gaussian/loop-transfer-recovery (LQG/LTR) design for an automatic landing controller for a typical commercial aircraft encountering a severe wind shear is presented. The airplane model is described, and the control objectives are outlined. Simulation results are presented, and the performance of the controller in handling the wind shear is evaluated
Keywords :
Kalman filters; aerospace simulation; aircraft landing guidance; closed loop systems; control system synthesis; controllers; linear quadratic Gaussian control; robust control; shear turbulence; wind; airplane model; automatic landing controller; commercial aircraft; control design; linear quadratic Gaussian controller; loop transfer recovery; performance; wind shear; Aerodynamics; Aerospace control; Aircraft; Airplanes; Automatic control; Control system synthesis; Neural networks; Nonlinear dynamical systems; Nonlinear equations; Robust control;
Conference_Titel :
System Theory, 1993. Proceedings SSST '93., Twenty-Fifth Southeastern Symposium on
Conference_Location :
Tuscaloosa, AL
Print_ISBN :
0-8186-3560-6
DOI :
10.1109/SSST.1993.522780
