期刊文献+

一种非线性自适应切换控制混合方法及其在倾转旋翼机上的应用 被引量:5

A nonlinear adaptive switching control blending method and its application to tiltrotor
原文传递
导出
摘要 为避免子控制器切换时控制量的跳变,提出了一种非线性自适应切换控制混合方法。针对输入输出反馈线性化子控制器在使用中存在的逆误差及模型不确定性,采用多层神经网络进行在线补偿,为实现此类非线性自适应子控制器的平滑切换,实际控制律采用各子控制律的凸组合,各组合系数值由切换参数确定。通过合适的设计参数选取与神经网络权值更新律设置,寻找到了闭环切换系统的公共Lyapunov函数,保证了此类系统在切换控制混合下的稳定性。在倾转旋翼机轨迹跟踪控制的应用中,设计了直升机模式、过渡模式与飞机模式的非线性子控制器,应用神经网络在线补偿与随短舱角的控制混合,仿真结果表明该方法具有对系统不确定性的鲁棒性及平滑切换的特性。 To avoid control signals of sub-controllers bumping at switching time,a nonlinear adaptive switching control blending method is presented.Multilayer neural-net is used to compensate the inversion error of feedback linearization controllers and unmodeled uncertainties.The convex combination of each sub-controller output is utilized as the online control signal in which the weight value of each sub-controller is determined by a switching parameter,and then the continuous and smooth switching can be achieved.A common Lyapunov function of the closed-loop switching control system is found by choosing design parameters and weights update laws of neural-net appropriately,then the stability of this system is guaranteed.With its application to tiltrotor trajectory tracking control,three sub-controllers are designed based on input-output feedback linearization for helicopter mode,transition mode and airplane mode,which are combined with neural-net online compensation and switching control blending by nacelle angle for all controllers.Simulation results show that this method is robust for plant uncertainties and has a smooth switching characteristic in mode conversions.
作者 王奇 吴文海
出处 《航空学报》 EI CAS CSCD 北大核心 2015年第10期3359-3369,共11页 Acta Aeronautica et Astronautica Sinica
基金 航空科学基金(20100785001)~~
关键词 非线性切换系统 平滑切换 神经网络 倾转旋翼机 飞行控制 switched nonlinear system smooth switching neural networks tiltrotor flight control
  • 相关文献

参考文献2

二级参考文献22

  • 1杨喜立,朱纪洪,黄兴李,胡春华,孙增圻.倾转旋翼飞机建模与仿真[J].航空学报,2006,27(4):584-587. 被引量:16
  • 2Foster M. The future evolution of the tihrotor [ R ]. AIAA- 2003-2652,2003.
  • 3Alli P, Nannoni F, Cical M. Erica: the european tihrotor design and critical technology projects [ R ]. AIAA-2003- 2515,2003.
  • 4Choi S, Kang Y, Chang S, et ah Development and conver- sion flight test of a small tihrotor unmanned aerial vehicle [ J]. Journal of Aircraft,2010,47(2) :730-732.
  • 5Carlson E B, Zhao Y J. Optimal city-center takeoff opera- tion of tiltrotor aircraft in one engine failure [ J ]. Journal of Aerospace Engineering,2004,17 ( 1 ) : 26-39.
  • 6Carlson E B, Zhao Y J. Prediction of tiltrotor height-veloc- ity diagrams using optimal control theory [ J ]. Journal of Aircraft, 2003,40 ( 5 ) : 896-905.
  • 7Kleinhesselink K M. Stability and control modeling of til- trotor aircraft [ D ]. College Park: University of Maryland, 2007.
  • 8Miller M, Narkiewicz J. Tihrotor modelling for simulation in various flight conditions[ J]. Journal of Theoretical and Applied Mechanics,2006,44 (4) : 881-906.
  • 9Gordon L J. Principles of helicopter aerodynamics [ M ]. 2nd ed. New York: Cambridge University Press, 2006: 95-96.
  • 10Harendra P B, Joglekar M J, Gaffey T M, et al. A mathe- matical model for real time-flight simulation of the Bell model 301 tilt rotor research aircraft model 301 [ R]. Bell Helicopter Company Report No. 301-099-001,1973.

共引文献2

同被引文献35

引证文献5

二级引证文献31

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