考虑作动器速率饱和的人机闭环系统稳定域

曹启蒙; 李颖晖; 徐浩军

考虑作动器速率饱和的人机闭环系统稳定域

空军工程大学航空航天工程学院, 西安 710038

基金项目: 国家自然科学基金资助项目(61074007)

详细信息

中图分类号: V328
计量
- 文章访问数: 1697
- HTML全文浏览量: 101
- PDF下载量: 728
- 被引次数: 0
出版历程
- 收稿日期: 2012-01-09
- 网络出版日期: 2013-02-28

Stability region for closed-loop pilot-vehicle system with actuator rate saturation

School of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi'an 710038, China

摘要

摘要: 针对作动器速率饱和引起的Ⅱ型驾驶员诱发振荡(PIO,Pilot Induced Oscillations)严重威胁先进战机飞行安全的问题,研究了计及作动器速率饱和的人机闭环系统稳定域.建立了考虑作动器速率饱和的人机闭环系统非线性模型,引入增广状态变量以及饱和度函数处理速率饱和环节,应用椭球体不变集估计人机闭环系统的稳定域,得到了稳定域估计的一般算法.通过时域仿真研究了所估计的稳定域的保守性,研究了驾驶员操纵增益以及作动器速率饱和值对稳定域的影响.结果表明:稳定域法物理意义清晰、结果直观,可用于人机闭环系统稳定性的评估.研究结果可为先进战机飞行控制系统的设计提供理论依据.
- 驾驶员诱发振荡 /
- 速率饱和 /
- 人机闭环系统 /
- 稳定域 /
- 椭球体不变集
Abstract: To solve advanced warplanes flight safety problem caused by category Ⅱ pilot induced oscillations(PIOs), the stability region of closed-loop pilot-vehicle system with actuator rate saturation was studied. The nonlinear model of closed-loop pilot-vehicle system was built. The augmented state variables and saturation degree function were introduced to address the rate saturation element. The ellipsoidal invariant sets were applied to estimate the stability region of closed-loop pilot-vehicle system. The stability region estimating algorithm was obtained. The stability region conservatism was investigated by time domain simulation and the effects of pilot control gain and rate saturation value on the stability region were researched. The results show that the stability region method has specific physical concept and illustrative results, and can be applied to evaluate the stability of closed-loop pilot-vehicle system. The results can provide a theoretical guidance for designing flight control systems of advanced warplanes.
- pilot induced oscillations(PIO) /
- rate saturation /
- closed-loop pilot-vehicle system /
- stability regions /
- ellipsoidal invariant sets

HTML全文

参考文献(9)

[1]	Dornhein M A. Report pinpoints factors leading to the Yf-22 crash[J] .Aviation Week and Space Technology,1992,137(19):53-54
[2]	高金源,李陆豫,冯亚昌.飞机飞行品质[M].北京:国防工业出版社,2003 Gao Jinyuan,Li Luyü,Feng Yachang.Aircraft handling qualities[M].Beijing:National Defence Industry Press,2003(in Chinese)
[3]	孟捷,徐浩军,李大伟.Gap准则在Ⅱ型PIO预测中的应用[J].北京航空航天大学学报,2010,36(9):1067-1070 Meng Jie,Xu Haojun,Li Dawei. Application of Gap criterion in prediction of category Ⅱ PIO[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36 (9) : 1067-1070 ( in Chinese)
[4]	Ossmann D, Heller M, Brieger O. Enhancement of the nonlinear OLOP-PIO-criterion regarding phase-compensated rate limiters .AIAA 2008-6207,2008
[5]	Klyde H D, McRuer T D, Myers T T. Pilot-induced oscillation analysis and prediction with actuator rate limiting[J]. Journal of Guidance, Control and Dynamics, 1997, 20(1): 81-89
[6]	Goman M G, Fedulova E V, Khramtsovsky A V. Maximum stability region design for unstable aircraft with control constraints .AIAA-96-3910,1996
[7]	Blanchini F. Set invariance in control[J]. Automatica,1999,35(11):1747-1767
[8]	Hu T S,Lin Z L.Exact characterization of invariance ellipsoids for single input linear systems subject toactuator saturation[J].IEEE Trans on Automatic Control,2002,47(1):164-169
[9]	魏爱荣,赵克友.运用线性反馈分析设计饱和线性系统[J].控制与决策,2005,20(1):59-60 Wei Airong,Zhao Keyou. Analysis and design for linear systems with saturation by linear feedback[J].Control and Decision,2005,20(1):59-60 (in Chinese)