期刊文献+

基于参考观测器的无人直升机航迹跟踪控制

Trajectory Tracking Control of Unmanned Helicopter Based on Reference Observer
下载PDF
导出
摘要 为实现无人直升机在工程应用中的精确航迹跟踪控制,从工程应用的角度提出基于参考观测器的航迹跟踪控制方法。根据航迹指令,通过参考观测器实时估算出无人直升机期望跟踪的状态量与控制量,作为航迹跟踪控制器的参考输入,再利用全状态反馈控制,操纵直升机跟踪期望的航迹,并以某型直升机为控制对象,在典型机动下进行航迹跟踪控制仿真验证。结果表明,该系统具有良好的航迹跟踪性能,且算法简单,易于实现。 A reference observer-based tracking control system is designed to achieve accurate trajectory tracking control in engineering application for an unmanned helicopter.According to the desired flight path,a real-time reference observer is developed to estimate the desired states and feed-forward control signals as the inputs of the tracking controller.Then the controller uses full-state feedback control method to realize trajectory tracking.A certain unmanned helicopter is chosen as the control plant,and the flight simulation is carried out in the typical maneuver of the helicopter.Simulation result shows the satisfactory performance of the system and the control approach is easy to be implemented in engineering for its simple algorithm.
作者 张瑾 袁锁中
出处 《兵工自动化》 2011年第2期58-61,共4页 Ordnance Industry Automation
关键词 无人直升机 航迹跟踪控制 观测器 最优控制 unmanned helicopter trajectory tracking observer optimal control
  • 相关文献

参考文献15

  • 1Snell S A,Enns D F,and Garrard W L.Nonlinear Control of a Supermaneuverable Aircraft[R].AIAA 89-3486-cp,1989.
  • 2Snell S A,Enns D F,and Garrard W L.Nonlinear inversion flight control for a super-maneuverable aircraft[J].AIAA Journal of Guidance,Control and Dynamics,1992,15(4):976-984.
  • 3Reiner J,Balas G J,and Garrard W L.Flight Control design using robust dynamic inversion and time-scale separation[J].Automatic,1996,32(11):1493-1540.
  • 4Snell S,and Stout P.Robust longitudinal control design using dynamic inversion and quantitative feedback theory[J].AIAA Journal of Guidance,Control and Dynamics,1997,20(5):933-940.
  • 5Shim H,Koo T,Hoffmann F,and Sastry S.A comprehensive study of control design for an autonomous helicopter[C].USA:Proc of the 37th IEEE Conference on Decision and Control,Florida,1998:3653-3658.
  • 6Dudgeon G and Gribble J.Helicopter attitude command attitude hold using individual channel analysis and design[J].AIAA Journal of Guidance,Control and Dynamics,1997,20(5):962-971.
  • 7Yang C D,Liu W H.NonlinearDecoupling Control for Hovering Helicopter[C] // Proc of the American Control Conf.Anchorage,2002:4353-4358.
  • 8Marcel Bergerman,Omead Amidi,James Ryan Miller,Nicholas Vallidis,and Todd Dudek.Cascade Position and Heading Control of a Robotic Helicopter[C].USA:Proc of the 2007 IEEE/ RSJ International Conference on Intelligent Robots and Systems,San Diego,CA,2007:135-140.
  • 9Michael Trentini,Jeff K.Pieper.Model-Following Control of a Helicopter in Hover[C].Proc of the 1995 IEEE International Conference on Control Applications,Dearborn,September,1996:7-12.
  • 10Bilal Ahmed,Hemanshu R.Pota,and Matt Garratt.Flight Control of a Rotary wing UAV-A Practical Approach[C].Proc of the 47th IEEE Conference on Decision and Control,Cancun,Mexico,2008:5042-5047.

二级参考文献12

  • 1S A Snell,D F Enns and W L Garrard.Nonlinear Control of a Supermaneuverable Aircraft[C].Proceedings of the AIAA Guidance,Navigation,and Control Conference,(AIAA 89-3486),Washington,DC,1989.
  • 2C Gao,R A Hess.Inverse simulation of large-amplitude aircraft maneuvers[J].Journal of Guidance,Control and Dynamics,1993,16(4).
  • 3R A Hess,C Gao,S H Wang.Generalized techniques for inverse simulation applied to aircraft maneuvers[J].Journal of Guidance,Control and Dynamics,1991,14(5).
  • 4S A Snell,D F Enns,L G William.Nonlinear inversion flight control for a supermaneuverable aircraft[R].AIAA 90-3406,1990.
  • 5S A Lane,D F Enns and W L Garrard.Flight control design using nonlinear inverse dynamics[J].Automatica,1988,24(4).
  • 6J Reiner,G J Balas,W L Garrard.Flight Control Design Using Robust Dynamic Inversion and Time-Scale Separation[J].Automatica,1996,3(2).
  • 7Byoung S Kim,Anthony J calise.Nolinear flight control using neural networks[J].Journal of Guidance,Control and Dynamics,1997,20(1).
  • 8J B Davidson,F J Lallman,W T Bundick.Real-Time Adaptive Control Allocation Applied to a High Performance Aircraft[C].5th SIAM Conference on Control & Its Application.2001.
  • 9Walker D J.On the structure of a two degree-of-freedom controller[J].International Journal of Control (S0020-7179),1996,63(6):1105-1127.
  • 10Anon.Aeronautical design standard ADS-33E handling qualities requirements for military helicopters[S].US Army,St.Louis,MO,2000.

共引文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部