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《Electronic Measurement Technology》 2019-03
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Line of sight stabilization method of unmanned aerial vehicle based on composite parallel control

Wang Xiu;Hou Honglu;Tang Rui;Ren Mengru;School of Optoelectronic Engineering, Xi'an Technological University;  
In order to improve the anti-disturbance ability of the unmanned aerial vehicle Line of sight stabilization platform, a method of visual axis stabilization for the quantitative feedback theory(QFT) and PID composite parallel control is proposed. First, the QFT stabilization controller is designed by loop shaping method, then the QFT is used as main controller and PID is applied to realize the dynamic compensation of QFT. Finally, the simulation experiment is carried out. The results show that the QFT and PID parallel control system reduces the step response stabilization time by 58% and the platform disturbance isolation by 75% compared with the independent QFT control system. The experimental results verify that the method can meet the requirements of the unmanned aerial vehicle for the stability of the visual axis and is superior to the QFT control method.
【Fund】: 陕西省教育厅重点实验室科研计划项目(15JS035);; 陕西省工业科技攻关项目(2016GY-051)资助
【CateGory Index】: V279
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【Citations】
Chinese Journal Full-text Database 9 Hits
1 XUN Pan-pan;HAN Chong-wei;ZHAO Yu-he;WANG Bao-hua;Northwest Institute of Mechanical and Electrical Engineering;;Research on Robust Control of Gun Servo System Based on Quantitative Feedback Theory[J];兵工学报;2015-10
2 WANG Ri-jun;BAI Yue;XU Zhi-jun;ZHAO Chang-jun;ZHANG Xin;TIAN Yan-tao;Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences;University of Chinese Academy of Sciences;School of Electrical and Information Technology,Changchun Institute of Technology;School of Telecommunication Engineering,Jilin University;;A composite disturbance compensation method for airborne platform based on improved disturbance observer[J];光电子·激光;2015-01
3 Shi Baolan;Fu Weixian;Beijing Institute of Space Systems Engineering;;Design of Missile Pitching Channel Attitude Control System Based on Quantitative Feedback Theory[J];导弹与航天运载技术;2013-05
4 WANG Fei,SHI Zhen,MA Wen-qiao(College of Automation,Harbin Engineering University,Harbin Heilongjiang 150001,China);Control of Hypersonic Vehicle Based on QFT+DI[J];计算机仿真;2013-06
5 WANG Xiang-zhou,LIN Wen-hui,LI Jian-fei(School of Automation,Beijing Institute of Technology,Beijing 100081,China);Design of Quantitative Feedback Controller with PID Loop for 2-DOF Stabilized Platform[J];北京理工大学学报;2012-07
6 HU Hong-jie1,2,WANG Yuan-zhe1,2 (1.School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China; 2.Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,China);Composite compensation control scheme for airborne opto-electronic platform[J];光学精密工程;2012-06
7 LU Cun-kan, MA Jun, YAN Jie (College of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China);Robust Controller Design for Hypersonic Vehicle Based on QFT[J];系统仿真学报;2010-03
8 ZHANG Fuxing,ZHU Rong,XIONG Wei,LIU Peng,LIU Xudong,ZHOU Zhaoying(State Key Laboratory of Precision Measurement Technology and Instruments,Department of Precision Instruments and Mechanology,Tsinghua University,Beijing 100084,China);Augmented-stability controller for micro air vehicle based on quantitative feedback theory[J];清华大学学报(自然科学版);2010-02
9 XIE Rong,WANG Xin-ming,LI Yan(College of Automation,Northwestern Polytechnical University,Xi'an 710072,China);Dynamic Inversion-PID Controller of a Supermaneuverable Aircraft[J];飞行力学;2009-02
【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 SUN Zhong-ting;Xuzhou Electromedchanical Engineering Department of Jiangsu United Vocational College;;Design Scheme of Airborne Computer System for MUAV in RTLinux[J];电脑知识与技术;2015-30
2 Lü Yongxi;Zhang Weiguo;Wang Minwen;Shi Jingping;Department of Automatic Control,Northwestern Polytechnical University;Science and Technology on Aircraft Control Laboratory;;An Improved Fuzzy Logic Unsteady Aerodynamics Modeling Method[J];西北工业大学学报;2015-06
3 XUN Pan-pan;HAN Chong-wei;ZHAO Yu-he;WANG Bao-hua;Northwest Institute of Mechanical and Electrical Engineering;;Research on Robust Control of Gun Servo System Based on Quantitative Feedback Theory[J];兵工学报;2015-10
4 WANG Ri-jun;BAI Yue;XU Zhi-jun;GONG Xun;ZHANG Xin;TIAN Yan-tao;Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Science;University of Chinese Academy of Science;School of Electrical and Information Technology,Changchun Institute of Technology;School of Telecommunication Engineering,Jilin University;;Fuzzy self-adjusting tracking control based on disturbance observer for airborne platform mounted on multi-rotor unmanned aerial vehicle[J];浙江大学学报(工学版);2015-10
5 HUANG Xiao-bo;SHAO Peng-yuan;State Key Laboratory of UAV Special Technology at Northnestem Polytechnical University;;A Control Design Method of UAV for Maneuver Flight[J];测控技术;2015-09
6 PAN Zheng-wei;XUE Ya-li;ZHANG Hong-xiang;School of Automation Engineering,Nanjing University of Aeronautics and Astronautics;;Dynamic Inverse Control of Super-Maneuverable Aircraft Based on Sliding Mode Observer and PI[J];电光与控制;2015-09
7 TAN Jian;ZHOU Zhou;ZHU Xiao-ping;ZHANG Le;National Key Laboratory of UAV Special Technology,Northwestern Polytechnical University;UAV Research Institute,Northwestern Polytechnical University;;Attitude control for flying wing unmanned aerial vehicles based on fractional order integral sliding-mode[J];控制理论与应用;2015-05
8 WANG Ri-jun;BAI Yue;XU Zhi-jun;ZHAO Chang-jun;ZHANG Xin;TIAN Yan-tao;Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences;University of Chinese Academy of Sciences;School of Electrical and Information Technology,Changchun Institute of Technology;School of Telecommunication Engineering,Jilin University;;A composite disturbance compensation method for airborne platform based on improved disturbance observer[J];光电子·激光;2015-01
9 PENG Yong-tao;LIU Lin;National Key Laboratory of Science and Technology on Aircraft Control,FACRI;;Real-time command generator design for UCAV's optimal loop maneuver[J];飞行力学;2015-01
10 LIU Zhen-hua;GUAN Ping;LIU Xiao-he;School of Automation,Beijing Information Science and Technology University;;Model predictive control for hypersonic aircrafts[J];北京信息科技大学学报(自然科学版);2014-05
【Secondary Citations】
Chinese Journal Full-text Database 10 Hits
1 FANG Chenxi;ZHANG Hui;YE Peiqing;LIANG Wenyong;LI Weiqian;Beijing Key Laboratory of Precision/Ultra-Precision Manufacturing Equipments and Control,Department of Mechanical Engineering,Tsinghua University;Gansu Engineering Research Center for CNC Machine Tool;;High-speed feed-rate planning with friction error constraints[J];清华大学学报(自然科学版);2014-06
2 LI Xian-tao;ZHANG Bao;MAO Da-peng;SUN Jing-hui;LI Jia-quan;SHEN Hong-hai;Key Laboratory of Airborne Optical Imaging and Measurement,Changchun Institute of Optics,Fine Mechanics and Physics,Chinese Academy of Sciences;Graduate University of Chinese Academy of Sciences;;The two-stage ADRC of aerial photoelectrical stabilized platform[J];光电子.激光;2013-12
3 CHEN Jie1,2 FANG Hao1,2 XIN Bin1,2 DENG Fang1,2 1.School of Automation,Beijing Institute of Technology,Beijing 100081 2.Key Laboratory of Intelligent Control and Decision of Complex Systems,Beijing 100081;Modeling,Optimization and Control in Ground-based Digital Weapon Systems[J];自动化学报;2013-07
4 FU Jin-bao1,2,3*,DING Ya-lin1,3,ZHONG Chong-liang1,2,3,LENG Xue1(1.Key Laboratory of Airborne Optical Imaging and Measurement,Changchun Institute of Optics, Fine Mechanics and Physics,Chinese Academy of Sciences,Changchun 130033,China; 2.University of Chinese Academy of Sciences,Beijing 100039,China; 3.Changchun Institute of Optics,Fine Mechanics and Physics, Chinese Academy of Sciences,Changchun 130033,China);Compensation controller with disturbance observer for forward image motion of aerial camera[J];光学精密工程;2013-06
5 DUAN Pengfei FAN Bin XIANG Weiguo (Beijing Institute of Space Mechanics & Electricity,Beijing 100076,China);Vibration Isolation Design and Test Analysis of Opti-electronic Platform for a UAV[J];航天返回与遥感;2012-05
6 LI Xiao-ning1,ZHAO Xian-feng1,HUANG Da-gui1,SHAO Wei2(1.School of Macaronis Engineering,University of Electronic Science and Technology of China,Chengdu Sichuan 611731,China;2.Institute of Chemical Materials,China Academy of Engineering Physics,Mianyang Sichuan 621900,China);Decoupling control for permanent magnet synchronous motor based on single neuron[J];控制理论与应用;2012-07
7 HU Hong-jie1,2,WANG Yuan-zhe1,2 (1.School of Automation Science and Electrical Engineering,Beihang University,Beijing 100191,China; 2.Science and Technology on Aircraft Control Laboratory,Beihang University,Beijing 100191,China);Composite compensation control scheme for airborne opto-electronic platform[J];光学精密工程;2012-06
8 ZHU Hai-rong1,2,LI Qi1,GU Ju-ping2,LI Jun-hong2(1.School of Automation,Southeast University,Nanjing 210096,China; 2.School of Electrical Engineering,Nantong University,Nantong 226019,China);Single-neuron adaptive PI control of the gyrostabilized platform based on disturbance compensation[J];电机与控制学报;2012-03
9 LI Jia-quan1,DING Ce1,2,KONG De-jie1,2,YIN Chuan-li1,DAI Ming1(1.Changchun Institute of Optics,Fine Mechanics and Physics, Chinese Academy of Sciences,Changchun 130033,China; 2.Graduate University of Chinese Academy of Sciences,Bejing 100039,China);Velocity based disturbance observer and its application to photoelectric stabilized platform[J];光学精密工程;2011-05
10 GUO Ya-jun,WANG Xiao-feng,MA Da-wei,LE Gui-gao(School of Mechanical Engineering,Nanjing University of Science and Technology,Nanjing 210094,Jiangsu,China);Application of Adaptive Backstepping Sliding Mode Controlin in Alternative Current Servo System of Rocket Gun[J];兵工学报;2011-04
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