DocumentCode :
553042
Title :
Disturbances analysis for a hypersonic vehicle based on adaptive fuzzy control
Author :
Zhao-Hua Yang ; Yun-shan Feng
Author_Institution :
Sch. of Instrum. Sci. & Opto-Electron. Eng., Beihang Univ., Beijing, China
Volume :
1
fYear :
2011
fDate :
26-28 July 2011
Firstpage :
123
Lastpage :
128
Abstract :
There are many different disturbances for hypersonic air vehicles due to complex flight environment and flight conditions of the high altitudes and Mach numbers. This paper analyses many kinds of disturbances such as aerodynamic interference, measurement noise, elevator disturbance and parametric uncertainty based on the fuzzy adaptive controller. Simulation results show that these disturbances obviously impact the flight tracking of height and velocity. However, the fuzzy adaptive controller is also able to effectively overcome these problems, and it has fine tracking performance and robustness.
Keywords :
Mach number; adaptive control; aerodynamics; aircraft control; fuzzy control; missiles; noise measurement; uncertain systems; Mach numbers; aerodynamic interference; elevator disturbance analysis; flight conditions; flight environment; flight tracking; fuzzy adaptive controller; hypersonic air vehicles; measurement noise; parametric uncertainty; Adaptation models; Aerodynamics; Atmospheric modeling; Elevators; Simulation; Uncertainty; Vehicles; adaptive; disturbance; fuzzy; hypersonic vehicle;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fuzzy Systems and Knowledge Discovery (FSKD), 2011 Eighth International Conference on
Conference_Location :
Shanghai
Print_ISBN :
978-1-61284-180-9
Type :
conf
DOI :
10.1109/FSKD.2011.6019542
Filename :
6019542
Link To Document :
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