期刊文献+

飞机自动着陆的一种非线性鲁棒控制器设计 被引量:2

A nonlinear robust controller designed for aircraft's automatic landing
下载PDF
导出
摘要 将一种直接基于非线性模型的带神经网络补偿信号的逆系统方法用于具有强非线性和受不确定扰动干扰的飞机自动着陆控制,并对神经网络补偿的方式进行了改进。采用神经网络补偿动态逆反馈线性化后伪系统的逆误差,使得非线性系统在参数受到摄动或外部扰动的情况下仍能保持良好的控制效果。可以证明该方法在理论上是收敛的,对于任意的状态初值和给定的期望输出信号,能控制到指定的精度。神经网络的权值是局部收敛的,同时大量仿真表明,经过较少的神经网络离线训练,即能够获得很好的控制效果。最后通过飞机着陆下滑段的仿真验证表明,该方法具有强的鲁棒性和良好的跟踪精度。 A neural network compensated inverse system method was proposed to control aircraft's automatic landing with strong nonlinearity and unknown perturbation, which was directly based on nonlinear model. The compensation mode of neural network was improved. The inversion error of pseudo linear systems was compensated by a neural network after dynamic inversion feedback linearization, thus good control performance was held by the nonlinear system with unprecise parameters and outside perturbation. The convergence of the method was proved theoretically. The given control precision can be satisfied with arbitrary initial state and given preference command. The neural networks' weights are locally converged, and it is confirmed by simulation that the method has a good control performance with little offline training of neural network. At last, simulation of aircraft's auto - landing in gliding mode shows that the method has strong robustness and good tracking precision.
出处 《电光与控制》 北大核心 2005年第6期20-24,共5页 Electronics Optics & Control
关键词 逆系统 神经网络 鲁棒性 飞行控制 非线性系统 inverse system neural networks robustness flight control nonlinear system
  • 相关文献

参考文献14

  • 1JUANG J G, CHIO J Z . Aircraft landing control based on fuzzy modeling networks[A]. Proceedings of the 2002 IEEE International Conference on Control Applications[C], 2002: 144-149. 被引量:1
  • 2IIGUNI,Y, AKIYOSHI H, ADACHI, N. An intelligent landing system based on a human skill model[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(3): 877-882. 被引量:1
  • 3CHE J, CHEN D G. Automatic landing control using H/sub infinity / control and stable inversion[A]. Proceedings of the 40th IEEE Conference on Decision and Control[C]. 2001: 241-246. 被引量:1
  • 4JUANG J G , CHANG H H, CHENG K C. Intelligent landing control using linearized inverse aircraft model[A].Proceedings of the 2002 American Control Conference[C]. 2002: 3269-3274. 被引量:1
  • 5LI Y, WANG Z F, SUNDARARAJAN N, et al. Neuro-Controllers for Aircraft Auto-Landing under Severe Wind Conditions[A]. Proceedings of the American Control Conference[C]. 2003: 1296-1301. 被引量:1
  • 6HOJJAT I, MEHRDAD P, NASSER S. Optimal neuro-controller in longitudinal autolanding of a commercial jet transport[A]. Proceedings of 2003 IEEE Conference on Control Applications[C], 2003: 492-497. 被引量:1
  • 7LI Y, SUNDARARAJAN N, SARATCHANDRAN P, et al. Robust neuro-H infinity controller design for aircraft auto-landing[J]. IEEE Transactions on Aerospace and Electronic Systems, 2004, 40(1): 158-167 被引量:1
  • 8JUANG J G, CHENG K C. Wind disturbances encountered during controlled landings using neural network approaches[A]. Proceedings of the 2001 IEEE International Conference on Control Applications CCA '01[C], 2001: 835-840. 被引量:1
  • 9NIEWOEHNER R J. KAMINER, I I. Design of an autoland controller for an F-14 aircraft using H/sub infinity / synthesis[J]. Journal of Guidance, Control, and Dynamics, 1996, 19(3): 656-663. 被引量:1
  • 10BALAKRISHNAN S N, BIEGA V. Adaptive-critic-based neural networks for aircraft optimal control[J]. Journal of Guidance, Control, and Dynamics,1996, 19(4): 893-898. 被引量:1

同被引文献12

  • 1洪耀伦.航空无线电导航原理[M].西安:空军通信学院,1980. 被引量:1
  • 2张忠兴,李晓明.无线电导航原理[M].西安:陕西科学技术出版社,1998. 被引量:1
  • 3QUINET D, ODUNAIYA S. Localizer receiver proximity and capture [ C]// IEEE 26th Digital Avionics System Conference, Ohio USA, 2007 : 4. C 2.1 - 4. C 2.8. 被引量:1
  • 4LENTMAIER M, KRACH B,JOST T,et al. Assessment of multipath in aeronautical environments [ R ]. ICAO - Report, 2008. 被引量:1
  • 5Iiguni Y,Akiyoshi H,Adachi N.An intelligent landing system based on a human skill model[J].IEEE Transactions on Aerospace and Electronic Systems(S0018-9251),1998,34(3):877-882. 被引量:1
  • 6Li Yan,Sundararajan N,Saratchandran P,et al.Robust neuro-controller design for aircraft auto-landing[J].IEEE Transactions on Aerospace and Electronic Systems(S0018-9251),2004,40(1):158-167. 被引量:1
  • 7Yan Li,Zhifeng Wang,Sundararajan N,et al.Fault tolerant neuro-controller design for aircraft auto-landing[C]// In:Proceedings of the 35th Southeastern Symposium on System Theory.2003:172-175. 被引量:1
  • 8Jun Che,Degang Chen.Automatic landing control using control and stable inversion[C]// In:Proceedings of the 40th IEEE Conference on Decision and Control.2001:241-246. 被引量:1
  • 9Jih-Gau Juang,Hao-Hsiang Chang,Kai Chung Cheng.Intelligent landing control using linearized inverse aircraft model[C]// In:Proceedings of the 2002 American Control Conference.2002:3269-3274. 被引量:1
  • 10刘玉洲.舰艇摇摆对雷达测向精度及工作方式的影响[J].舰船电子对抗,2002,25(2):18-21. 被引量:23

引证文献2

二级引证文献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