TY - JOUR
T1 - Integral sliding mode nonlinear controller of electrical-hydraulic flight simulator based on neural network
AU - Han, Songshan
AU - Jiao, Zongxia
AU - Wang, Chengwen
AU - Shi, Yan
PY - 2014/3
Y1 - 2014/3
N2 - For the feature that high-accuracy electrical-hydraulic flight simulator (EHFS) is highly nonlinear and contains parametric uncertainties and uncertain nonlinearities, an integral sliding mode nonlinear robust controller based on radial basis function (RBF) neural network was proposed. The adaptive RBF neural network was adopted to eliminate the effect of parametric uncertainties and uncertain nonlinearities. By reducing the gain of switching function in sliding mode controller, chattering phenomenon could be minimized significantly. The steady state error from external disturbances could be eliminated by integral sliding control law, which was divided into an equivalent control law and a hitting control law. Equivalent control law was designed to keep the system sliding along the sliding surface. Hitting control law was applied to drive the representation point of the state space onto the sliding surface. The globally asymptotic stability of developed controller was proven via Lyapunov analysis. Comparative experimental results demonstrate the effectiveness of the proposed algorithm.
AB - For the feature that high-accuracy electrical-hydraulic flight simulator (EHFS) is highly nonlinear and contains parametric uncertainties and uncertain nonlinearities, an integral sliding mode nonlinear robust controller based on radial basis function (RBF) neural network was proposed. The adaptive RBF neural network was adopted to eliminate the effect of parametric uncertainties and uncertain nonlinearities. By reducing the gain of switching function in sliding mode controller, chattering phenomenon could be minimized significantly. The steady state error from external disturbances could be eliminated by integral sliding control law, which was divided into an equivalent control law and a hitting control law. Equivalent control law was designed to keep the system sliding along the sliding surface. Hitting control law was applied to drive the representation point of the state space onto the sliding surface. The globally asymptotic stability of developed controller was proven via Lyapunov analysis. Comparative experimental results demonstrate the effectiveness of the proposed algorithm.
KW - Electrical-hydraulic flight simulator
KW - Hydraulic servo control
KW - Integral sliding mode
KW - Radial basis function neural network
KW - Robust controller
UR - https://www.scopus.com/pages/publications/84898676782
U2 - 10.13700/j.bh.1001-5965.2013.0688
DO - 10.13700/j.bh.1001-5965.2013.0688
M3 - 文章
AN - SCOPUS:84898676782
SN - 1001-5965
VL - 40
SP - 321
EP - 326
JO - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
JF - Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
IS - 3
ER -