Title :
Fuzzy model reference learning control for aircraft pitch autopilot design
Author :
Yuan, Yuman ; Feng, Yuguang ; Gu, Wenjin
Author_Institution :
Dept. of Autom. Control, Naval Aeronaut. Eng. Inst., China
Abstract :
In this paper, the idea of fuzzy model reference learning control(FMRLC) technique for missile autopilot design is introduced. This controller utilizes a learning mechanism, which observes the plant outputs and adjusts the rules in a direct fuzzy controller, so that the overall system behaves like a "reference model" which characterizes the desired behaviour. The performance of the FMRLC based missile autopilot is demonstrated by simulation for various conditions with structure uncertainties.
Keywords :
aircraft control; attitude control; control system synthesis; fuzzy control; learning (artificial intelligence); missile control; model reference adaptive control systems; uncertain systems; FMRLC based missile autopilot; aircraft pitch autopilot design; fuzzy controller; fuzzy model reference learning control; learning mechanism; missile autopilot design; structure uncertainty; Adaptive control; Aerospace control; Aircraft; Automatic control; Control systems; Error correction; Fuzzy control; Fuzzy systems; Missiles; Nonlinear control systems;
Conference_Titel :
Control, Automation, Robotics and Vision Conference, 2004. ICARCV 2004 8th
Print_ISBN :
0-7803-8653-1
DOI :
10.1109/ICARCV.2004.1469454
