Zhang Jiayi, Luo Xiling, Huang Zhiganget al. Optimization of multi-mode motion estimation algorithm in H.264[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 140-143. (in Chinese)
Citation: Cao Qimeng, Li Yinghui, Xu Haojunet al. Stability region for closed-loop pilot-vehicle system with actuator rate saturation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 215-219. (in Chinese)

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

  • Received Date: 09 Jan 2012
  • Publish Date: 28 Feb 2013
  • 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.

     

  • [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)
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