期刊文献+

基于改进差分进化算法的PIO预测评估方法 被引量:2

Prediction and evaluation method for PIO based on modified differential evolution
原文传递
导出
摘要 提出了一种基于改进差分进化算法的驾驶员诱发振荡(PIO)预测评估方法。针对基本差分进化算法收敛慢、易陷入局部最优的问题,提出了基于混沌理论与高斯扰动的改进型差分进化算法。在此基础上,构建了基于改进差分进化算法的PIO预测评估流程与实施步骤,建立了基于速率限制的人机闭环系统模型。实例计算结果表明,该方法克服了传统评估方法的缺陷,可在多参数摄动情况下对PIO进行快速准确的评估。 This paper presents the prediction and evaluation method for pilot induced oscillations (PIO) based on modified differential evolution. For the problem of slow search and premature convergence in the basic differential evolution, a new modified method based on chaos theory and Gaussian disturbance is proposed. And then the process to evaluate the pilot induced oscillations is put forward. The human ma- chine system model based on rate-limit is set up. The results show that the method can be used to achieve satisfied results in parameters perturbation.
出处 《飞行力学》 CSCD 北大核心 2014年第1期74-77,83,共5页 Flight Dynamics
基金 国防预研基金资助(51327020104)
关键词 PIO 差分进化算法 速率限制 人机系统 PIO differential evolution rate-limit human machine system
  • 相关文献

参考文献6

二级参考文献30

  • 1宁国栋,方振平.Neal-Smith时域PIO预测准则及应用[J].北京航空航天大学学报,2005,31(4):407-411. 被引量:9
  • 2刘林,车军,唐强,陈宗基.现代飞行控制律评估与确认先进方法研究[J].飞行力学,2007,25(1):1-4. 被引量:5
  • 3刘林,纪多红,唐强.ν-gap度量及其在飞行控制律评估中的应用[J].航空学报,2007,28(4):930-934. 被引量:2
  • 4McRuer D T. Aviation safety and pilot control,understanding and preventing unfavorable pilot-vehicle interactions [ M ]. Washington D. C : National Academy Press, 1997.
  • 5Gilbreath G P. Prediction of pilot-induced oscillations (PIO) due to actuator rate limiting using the open-loop onset point (OLOP) criterio[ D ]. Wright-Patterson AFB OH : Department of the Air Force Air University,Air Force Institute of Technology,2001.
  • 6Mitchell D G, Klyde D H. Testing for pilot-induced oscillations [ R]. AIAA-2005-5811,2005.
  • 7Witte J B. An investigation relating longitudinal pilot-induced oscillation tendency rating to describing function predictions for rate-limited actuators [ D ]. Wright-Patterson AFB OH : Department of the Air Force Air University ,Air Force Institute of Technology ,2004.
  • 8Witte J B. An investigation relating longitudinal pilot-in- duced oscillation tendency rating to describing function predictions for rate-limited actuators [ D ]. America: Air Force Institute of Technology,2004.
  • 9James Hanley G. A comparison of nonlinear algorithms to prevent pilot-induced oscillations caused by actuator rate limiting [ D ]. America: Air Force Institute of Technology, 2003.
  • 10Mitchell Klyde. Testing for pilot-induced oscillations [ C]//AIAA Atmospheric Flight Mechanics Conference America,2005:98-111.

共引文献10

同被引文献26

  • 1丛爽,邓娟.MATLAB环境下的模型预测控制理论的应用[J].计算机工程与应用,2005,41(16):196-198. 被引量:7
  • 2郭晓辉,宋笔锋.红外干扰下飞机击中概率计算[J].电光与控制,2005,12(6):5-7. 被引量:6
  • 3王斯福,刘永才,关世义,强文义,张克.伴飞诱饵支援条件下无人飞行器协同作战效能研究[J].宇航学报,2007,28(2):498-502. 被引量:18
  • 4Liang X H, Yamada K, Sakamoto N, et al. Model predictive controller design to suppress rate-limiter-based pilot-induced oscillations[ J]. Ja- pan Society of Aeronautical Space Sciences Transactions, 2007, 49 (166) : 239 - 245.
  • 5Duda H. Prediction of pilot-in-the-loop oscillations due to rate saturation[J]. Journal of Guidance, Control, and Dynamics, 1997, 20 (3) : 581 -587.
  • 6Liebst B S, Chapa M J, Leggett D B. Nonlinear prefilter to prevent pilot-induced oscillations due to actuator rate limiting[ J ]. Journal of Guid- ance, Control, and Dynamics, 2002, 25 (4) : 740 - 747.
  • 7Henley J G. A comparison of nonlinear algorithms to prevent pilot-induced oscillations caused by actuator rate limiting [ D ]. Maxwell, AL, USA : Air University, 2003 : 1 - 84.
  • 8Kapila V, Valluri S. Model predictive control of systems with actuator amplitude and rate saturation[C]//Proceedings of the 37th IEEE Con- ference on Decision and Control. Piscataway, NJ, USA: IEEE, 1998:1396 -1401.
  • 9Liang X H. Model predictive controller design to suppress rate-limiter-based pilot induced oscillations[ D ]. Nagoya: Nagoya University, 2006.
  • 10McRuer D T. Pilot-induced oscillations and human dynamic behavior[ M]. Washington, USA: NASA, 1995.

引证文献2

二级引证文献2

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