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《Electric Machines and Control》 2010-09
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Robust control system design for a aducted fan unmanned aerial vehicle

LI Yuan-wei,WANG Chang-hong,YI Guo-xing,XI Bo-qi (Space Control and Inertial Technology Research Center,Harbin Institute of Technology,Harbin 150080,China)  
The flight attitude control system for the small size ducted fan unmanned aerial vehicle (UAV) is presented.Firstly,the mathematic model for the UAV is constructed from the forces and moments analysis of the vehicle,and the derived nonlinear model is linearized in the hovering flight condition.Then the robust flight attitude controller based on this linear model is designed to deal with the parameter uncertainty and external disturbance which is due to the compact configuration.The validity of the controller is verified by the simulation results,and also the controller is applied in the flight testing.The results show that the vehicle with the controller has a good performance of operation stability.
【Fund】: 国防预研资助项目(51309030102)
【CateGory Index】: V249.1
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【Citations】
Chinese Journal Full-text Database 2 Hits
1 LI Jian-bo, GAO Zheng, TANG Zheng-Fei, LU Yang (College of Aerospace Engineering, Nanjing University of Aeronautics & Astronautics,Nanjing,210016,China);Experimental Investigation on Lift and Drag of Ducted Fan System[J];Journal of Nanjing University of Aeronautics & Astronautics;2004-02
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【Co-citations】
Chinese Journal Full-text Database 10 Hits
1 FAN Ning-jun, XU Jia, YANG Ji-wei(School of Mechatronical Engineering,Beijing Institute of Technology,Beijing 100081,China);Numerical Study on Aerodynamic Characteristics of Ducted Fan Aircraft[J];北京理工大学学报(英文版);2010-01
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10 WANG Hong-qiang1,WANG Dao-bo1,Duan Hai-bin2(1.College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;2.School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,Beijing 100083);Stability and control analysis of rotor/ducted-fan based unmanned helicopter[J];Journal of Harbin Institute of Technology;2009-07
China Proceedings of conference Full-text Database 2 Hits
1 Tan Weirong Huang Shuilin Xu Guohua (National Key Laboratory of Rotorcraft Aeromechanics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China);Analysis on Aerodynamic Characteristics of Helicopter Ducted Taft Rotor[A];[C];2008
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