DocumentCode
506764
Title
RBF-based backstepping control of semi-active landing gear system with solenoid valve actuator
Author
Wu, Dongsu ; Gu, Hongbin ; Liu, Hui
Author_Institution
Coll. of Civil Aviation, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Volume
2
fYear
2009
fDate
20-22 Nov. 2009
Firstpage
858
Lastpage
863
Abstract
In this paper, we present a RBF-based backstepping scheme for the semi-active control of landing gear system using high speed solenoid valve actuator. The full dynamics of a novel semi-active shock strut including solenoid valve are considered. The proposed nonlinear controller is based on a hierarchical structure which contains three loops. The outer loop computes the expected optimal strut force on both touchdown and taxiing situation. The middle loop realizes the tracking of optimal strut force via backstepping design method and uses a RBF network to approximate the unmodelled nonlinear dynamics. The inner loop is responsible for precise tracking of valve current. A rigorous proof of stability is given and simulations are conducted on both touchdown and taxiing conditions to verify performance of proposed controller.
Keywords
actuators; aircraft control; gears; neurocontrollers; nonlinear control systems; radial basis function networks; stability; RBF-based backstepping control; hierarchical structure; nonlinear controller; semiactive landing gear system; semiactive shock strut; solenoid valve actuator; system stability; Actuators; Backstepping; Control systems; Design methodology; Electric shock; Gears; Nonlinear dynamical systems; Solenoids; Tracking loops; Valves; backstepping; landing gear; radial basis function network; semi-active control; solenoid valve;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computing and Intelligent Systems, 2009. ICIS 2009. IEEE International Conference on
Conference_Location
Shanghai
Print_ISBN
978-1-4244-4754-1
Electronic_ISBN
978-1-4244-4738-1
Type
conf
DOI
10.1109/ICICISYS.2009.5358274
Filename
5358274
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