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