Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Acta Aeronautica et Astronautica Sinica》 2011-05
Add to Favorite Get Latest Update

Design of Sliding Mode Controller Based on SMDO and Its Application to Missile Control

ZENG Xianfa1,WANG Jieyao2,WANG Xiaohu1,,WANG Tiejun1 1.Beijing Institute of Control & Electronics Technology,Beijing 100038,China 2.School of Astronautics,Harbin Institute of Technology,Harbin 150001,China  
A sliding mode controller(SMC) design approach based on the sliding mode disturbance observer(SMDO) is proposed.A class of cascade multiple-input multiple-output(MIMO) nonlinear system is separated into outer and inner loops based on the singular perturbation principle,and the controllers are designed in the two loops respectively.The robustness of the traditional saturation-function-based sliding mode controller is analyzed in the outer loop,and it is found to be weak in the presence of disturbances.To overcome this problem,together with the nominal sliding mode control law,SMDOs based on the super-twisting algorithm are designed to estimate and compensate for disturbances.Finally,the approach is applied to a missile control system design.The simulation results demonstrate that SMDO-based sliding mode controller(SMDO-SMC) effectively improves both the robustness and control performance of the control system.
【CateGory Index】: V448.22
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
【Citations】
Chinese Journal Full-text Database 2 Hits
1 Zeng Xianfa Zhang Lei Shen Gongzhang (School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);Design of control systems for missiles based on dynamic inversion and decentralized control[J];Journal of Beijing University of Aeronautics and Astronautics;2007-11
2 DING Shi-hong, LI Shi-hua(School of Aulomation, Southeast University, Nanjing 210096, China);Finite Time Tracking Control of Spacecraft Attitude[J];Acta Aeronautica Et Astronautica Sinica;2007-03
【Secondary Citations】
Chinese Journal Full-text Database 5 Hits
1 Li Yang Chen Wanchun(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China);Design and simulation of BTT nonlinear controller for hypersonic vehicle[J];Journal of Beijing University of Aeronautics and Astronautics;2006-03
2 MA Ke-mao, DONG Zhi-yuan (Simulation Center, Harbin Institute of Technology, Harbin 150001, China);Variable Structure Attitude Control of Spacecraft Large Angle Maneuver Flight[J];Flight Dynamics;2004-02
3 LI Shi-hua, TIAN Yu-ping(Department of Automatic Control, Southeast University, Nanjing 210096, China. );Finite Time Tracking Control Algorithm for Nonholonomic Mobile Robots[J];Control and Decision;2005-07
4 WU Tian-bao,HUANG Xian-lin,LU Hong-qian,BAN Xiaojun (Department of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,China);Design of a TF/TA controller for cruise missile using nonlinear dynamic inversion[J];Journal of Astronautics;2004-03
5 CHEN Jin-li~1, LI Dong-hai~2, SUN Xian-fang~1 (1 . School of Automation Science and Electronic Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China; 2. Department of Thermal Engineering, Tsinghua University, Beijing 100084, China);Nonlinear Robust Decentralized Controller Design for Spacecraft Attitude Control System[J];Journal of Astronautics;2006-01
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved