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微扑翼飞行机器人姿态反演自适应模糊控制 被引量:2

Adaptive Fuzzy Control of Attitude of the Flapping-wing Micro Air Vehicles Based on Backstepping
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摘要 研究微扑翼飞行机器人姿态控制优化问题,因扑翼飞行的复杂性、系统的非线性、时变参数以及各种干扰而极具挑战性。为了提高系统姿态稳定性,提出了一种反演自适应模糊控制策略,针对传统反演控制律设计的不足之处,对微扑翼飞行机器人控制律设计中需要知道被控对象精确模型信息的部分,采用模糊控制法去逼近,从而实现了无需微扑翼飞行器精确模型的全新控制律,避免了因建模误差对控制带来的不良影响,并在此基础上证明了系统的稳定性。仿真结果证实了控制方法的有效性。 The attitude control of Flapping-wing Micro Air Vehicles is very challenging owing to the complex flight process,and the heavy difficulty is that the system embodies nonlinearity,time varying parameters,and all kinds of disturbances.To control the attitude movement effectively,an adaptive fuzzy control strategy based on backstepping is contrived by analyzing the disadvantage of common backstepping.The method overcomes the impact of the modeling error on the control system.Theoretical result is supported by simulation of the adaptive fuzzy control of FMAV on backstepping,and the validity of the proposed method is verified.
出处 《计算机仿真》 CSCD 北大核心 2011年第5期80-84,共5页 Computer Simulation
关键词 微扑翼飞行机器人 姿态控制 反演控制 模糊控制 Flapping-wing micro air vehicle Attitude control Backstepping Fuzzy control
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参考文献7

  • 1J M Micheal, M S Francis. Micro air vehicles-toward a new di- mension in flight[ R]. US DARPA/TI'O Report, 1997.
  • 2H Y Wu, Z Y Zhou, D Sun. Autonomous hovering control and test for micro air vehicle[ C] . Proceedings of the 2003 IEEE In- ternational Conference on Robotics & Automation. Taipei, 2003.
  • 3S P Sane, M H Dickinson. The control of flight force by a flapping wing: Lift and drag production [ J ]. The Journal of experimental Biology, 2001, (204) :2607-2626.
  • 4L Schenato, D Campolo, S Sastry. Controllability issues in flap- ping flight for biomimetic Micro Aerial Vehicles (MAVs) [ C ]. Proceedings of the 42nd IEEE International Conference on Decision & Control. Mall/, Hawaii, USA, 2003.
  • 5刘金琨.机器人控制系统的设计与MATLAB仿真[M].北京清华大学出版社.2008.
  • 6段洪君,史小平.扑翼微型飞行器飞行姿态模型研究[J].航空动力学报,2007,22(8):1285-1289. 被引量:7
  • 7史小平,段洪君.扑翼微型飞行器非线性H∞姿态控制(英文)[J].系统仿真学报,2007,19(19):4499-4503. 被引量:3

二级参考文献24

  • 1刘岚,方宗德,侯宇,傅卫平,吴立言.微型扑翼飞行器的气动建模分析与试验[J].航空动力学报,2005,20(1):22-28. 被引量:15
  • 2Khan Z A,Agrawal S K.Force and moment characterization of flapping wings for micro air vehicle application[C]// In American Control Conference.June 8-10,Portland or USA:2005:1515-1520.
  • 3Lasek M,Pietrucha J,Zlocka M,et al.Analogies between rotary and flapping wings from control theory point of view[R].AIAA-2001-4002.
  • 4Sane S P,Dickinson M H.The aerodynamic effects of wing rotation and a revised quasi-steady model of flapping flight[J].Journal of Experimental Biology,2002,205:1087-1096.
  • 5Balint C N,Dickinson M H.Neuromuscular control of aerodynamic forces and moments in the blowfly,Calliphora vicina[J].Journal of Experimental Biology,2004,207:3813-3838.
  • 6Masashi H.Calculation method for optimal circulation distribution on a finite span flapping wing[R].AIAA-2002-3414.
  • 7Sane S P,Dickinson M H.The control of flight force by a flapping wing:lift and drag production[J].Journal of Experimental Biology,2001,204:2607-2626.
  • 8Schenato L,Campolo D,Sastry S.Controllability lssues in flapping flight for biomimetic micro aerial vehicles (MAVs)[C]//In Proceedings of the 42nd IEEE International Conference on Decision & Control.December,Maui,Hawaii USA:2003:6441-6447.
  • 9Lasek M,Pietrucha J,Sibilski K.Micro air vehicle maneuvers as a control problem of flexible flapping wings[R].AIAA-2002-0526.
  • 10Madangopal R,Khan Z A,Agrawal S K.Energetics based design of small flapping wing air vehicle[J].IEEE/ASME Transactions on Mechatronics,2006,11(4):433-438.

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