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Unscented Kalman-filter-based sliding mode control for an underwater gliding snake-like robot 期刊论文  OAI收割
Science China Information Sciences, 2020, 卷号: 63, 期号: 1, 页码: 1-13
作者:  
Tang JG(唐敬阁);  Li B(李斌);  Chang J(常健);  Zhang AQ(张艾群)
  |  收藏  |  浏览/下载:60/0  |  提交时间:2020/01/11
Digital Sliding Mode Control via a Novel Reaching Law and Application in Shipborne Electro-Optical Systems 期刊论文  OAI收割
Ieee Access, 2019, 卷号: 7, 页码: 139870-139884
作者:  
J.Q.Zhang;  Y.K.Liu;  F.J.Zhang;  S.J.Gao;  C.S.Han
  |  收藏  |  浏览/下载:31/0  |  提交时间:2020/08/24
Control Technology of Ground-Based Laser Communication Servo Turntable via a Novel Digital Sliding Mode Controller 期刊论文  OAI收割
Applied Sciences-Basel, 2019, 卷号: 9, 期号: 19, 页码: 19
作者:  
J.Q.Zhang;  Y.K.Liu;  S.J.Gao;  C.S.Han
  |  收藏  |  浏览/下载:23/0  |  提交时间:2020/08/24
Sliding Mode Control of Servo Motor Based on Novel Reaching Law 会议论文  OAI收割
Wuhan, China, July 25-27, 2018
作者:  
Zhang T(张涛);  Wang, Dazhi;  Wang, Anna;  Jin, Xin
  |  收藏  |  浏览/下载:36/0  |  提交时间:2018/12/25
Research on model reference sliding mode control in roll stabilization of aerocraft (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Chu H.-R.
收藏  |  浏览/下载:46/0  |  提交时间:2013/03/25
Aimed at aerospace roll stabilization  control arithmetic based on model reference sliding mode variable structure theory and chattering reduction arithmetic are formulated. Correctness and validity of arithmetic are analyzed. With flight dynamics  the roll-loop mathematic model and reference model are established. Sliding hyperplane is deduced based on model reference sliding mode variable structure theory. Combing with reaching law  control law is derived  and stability of roll-loop is analyzed. Chattering of aileron instructions is alleviate by using boundary layer approach. Digital flying simulation result shows that variable structure control arithmetic realized roll stabilization control  the roll angle is less than 5.3 under powered flight  and that of unpowered flight is less than 0.5  respectively. The command fin angle is less than 1.5. High frequency chattering of fin command nearby the minimum velocity was trailed off by chattering reduction arithmetic. The sliding mode control arithmetic show good performance when aerodynamic coefficients varies 20%. The control arithmetic is easy to be implemented for its simplicity. 2011 IEEE.  
The application of the discrete sliding mode control based on state observer in aerial camera (EI CONFERENCE) 会议论文  OAI收割
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
作者:  
Zhang X.;  Zhang X.;  Zhang X.
收藏  |  浏览/下载:28/0  |  提交时间:2013/03/25
Algorithm research of target acquisition for TV tracking system based on Sliding Mode Control (EI CONFERENCE) 会议论文  OAI收割
2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010, August 20, 2010 - August 22, 2010, Chengdu, China
Wu P.; Gao H.-B.
收藏  |  浏览/下载:32/0  |  提交时间:2013/03/25
Target acquisition algorithm based on Sliding Mode Control (SMC) is proposed for TV tracking system. Target acquisition capability and performance are both improved  attributing to overcoming the deficiencies of traditional linear control. In this paper  sliding surface with variable coefficient and continuous control law without switching is introduced in the SMC controller design. The improved SMC shows better performance compared to basic SMC  and full-field acquisition with rapid response and non-overshoot is achieved. The simulation of acquisition shows that  the system can acquire a target passing through the view field of 1.53 in the width with an uniform speed of 15 /s  while the whole process is in a short settling time and chattering-free  and the reaching segment has no overshoot. 2010 IEEE.  
Adaptive sliding mode control for airborne Opto-Electronic platform servo system (EI CONFERENCE) 会议论文  OAI收割
7th International Conference on Machine Learning and Cybernetics, ICMLC, July 12, 2008 - July 15, 2008, Kunming, China
Wang C.-X.; Liu J.-H.; Shen H.-H.; Dai M.
收藏  |  浏览/下载:29/0  |  提交时间:2013/03/25
The novel presents an adaptive reaching law sliding mode controller to slove a class of uncertain systems.The Airborne Opto-Electronic Platform sliding model is employed to represent a class of complex uncertain system. The control is based on reaching law control. Discrete time implementation of the sliding mode control strategy is considered in the paper  since it is more appropriate for practical applications. It is shown that the robustness of the sliding mode control method is constrained by sampling time. Design of the adaptive reaching law based on a discrete expotential reaching law concept is given  which to design a new sliding mode controller based on Lyapunov stability theory. The global asymptotic stability is guaranteed. An example with simulation results is given to illustrate the effectiveness of the proposed method. 2008 IEEE.