A journal of IEEE and CAA , publishes high-quality papers in English on original theoretical/experimental research and development in all areas of automation
Volume 2 Issue 2
Apr.  2015

IEEE/CAA Journal of Automatica Sinica

  • JCR Impact Factor: 11.8, Top 4% (SCI Q1)
    CiteScore: 17.6, Top 3% (Q1)
    Google Scholar h5-index: 77, TOP 5
Turn off MathJax
Article Contents
Delong Hou, Qing Wang and Chaoyang Dong, "Output Feedback Dynamic Surface Controller Design for Airbreathing Hypersonic Flight Vehicle," IEEE/CAA J. of Autom. Sinica, vol. 2, no. 2, pp. 186-197, 2015.
Citation: Delong Hou, Qing Wang and Chaoyang Dong, "Output Feedback Dynamic Surface Controller Design for Airbreathing Hypersonic Flight Vehicle," IEEE/CAA J. of Autom. Sinica, vol. 2, no. 2, pp. 186-197, 2015.

Output Feedback Dynamic Surface Controller Design for Airbreathing Hypersonic Flight Vehicle

Funds:

This work was supported by Natural National Science Foundation of China (61273083, 61374012).

  • This paper addresses issues related to nonlinear robust output feedback controller design for a nonlinear model of airbreathing hypersonic vehicle. The control objective is to realize robust tracking of velocity and altitude in the presence of immeasurable states, uncertainties and varying flight conditions. A novel reduced order fuzzy observer is proposed to estimate the immeasurable states. Based on the information of observer and the measured states, a new robust output feedback controller combining dynamic surface theory and fuzzy logic system is proposed for airbreathing hypersonic vehicle. The closedloop system is proved to be semi-globally uniformly ultimately bounded (SUUB), and the tracking error can be made small enough by choosing proper gains of the controller, filter and observer. Simulation results from the full nonlinear vehicle model illustrate the effectiveness and good performance of the proposed control scheme.

     

  • loading
  • [1]
    Chavez F R, Schmidt D K. Uncertainty modeling for multivariablecontrol robustness analysis of elastic high-speed vehicles. Journal of Guidance, Control, and Dynamics, 1999, 22(1):87-95
    [2]
    Zong Q, Ji Y H, Zeng F L, Liu H L. Output feedback backstepping control for a generic hypersonic vehicle via small gain theorem. Aerospace Science and Technology, 2012, 23(1):409-417
    [3]
    Bolender M A, Doman D B. Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle. Journal of Spacecraft and Rockets, 2007, 44(2):374-387
    [4]
    Sun Chang-Yin, Mu Chao-Xu, Yu Yao. Some control problems for near space hypersonic vehicles. Acta Automatica Sinica, 2013, 39(11):1901-1913(in Chinese)
    [5]
    Bao Wei-Min. Present situation and development tendency of aerospace control techniques. Acta Automatica Sinica, 2013, 39(6):609-702(in Chinese)
    [6]
    Dickeson J J, Rodriguez A A, Sridharam S, Benavides J, Soloway D. Decentralized control of an air-breathing scramjet-powered hypersonic vehicle. In:Proceedings of the 2009 AIAA Guidance, Navigation and Control Conference. Chicago, IL:AIAA, 2009. AIAA-2009-6281
    [7]
    Groves K P, Sigthorsson D O, Serrani A, Yurkovich S, Bolender M A, Doman D B. Reference command tracking for a linearized model of an air-breathing hypersonic vehicle. In:Proceedings of the 2005 AIAA Guidance, Navigation, and Control Conference. San Francisco, CA:AIAA, 2005. AIAA-2005-6144
    [8]
    Lind R, Buffington J, Sparks A. Multi-loop aeroservoelastic control of a hypersonic vehicle. In:Proceedings of the 1999 AIAA Guidance, Navigation, and Control Conference. Portland, OR:AIAA, 1999. AIAA-99-4123
    [9]
    Rick L. Linear parameter-varying modeling and control of structural dynamics with aerothermoelastic effects. Journal of Guidance, Control, and Dynamics, 2002, 25(4):733-739
    [10]
    Wilcox Z D, Mackunis W, Bhat S, Lind R, Dixon W E. Lyapunov-based exponential tracking control of a hypersonic aircraft with aerothermoelastic effects. Journal of Guidance, Control, and Dynamics, 2010, 33(4):1213-1224
    [11]
    Hu X, Wu L, Hu C, Gao H. Fuzzy guaranteed cost tracking control for a flexible air-breathing hypersonic vehicle. IET Control Theory and Applications, 2012, 69(4):1238-1249
    [12]
    Wang Q, Stengel R F. Robust nonlinear control of a hypersonic aircraft. Journal of Guidance, Control, and Dynamics, 2000, 23(4):577-585
    [13]
    Xu H J, Mirmirani M D, Ioannou P A. Adaptive sliding mode control design for a hypersonic. Journal of Guidance, Control, and Dynamics, 2004, 27(5):829-838
    [14]
    Hu X X, Wu L G, Hu C H, Gao H J. Adaptive sliding mode tracking control for a flexible air-breathing hypersonic vehicle. Journal of the Franklin Institute, 2012, 349(2):559-577
    [15]
    Gao G, Wang J Z. Reference command tracking control for an airbreathing hypersonic vehicle with parametric uncertainties. Journal of The Franklin Institute, 2013, 350(5):1155-1188
    [16]
    Fiorentini L, Serrani A, Bolender M, Doman D B. Nonlinear robust adaptive control of flexible air-breathing hypersonic vehicles. Journal of Guidance, Control, and Dynamics, 2009, 32(2):401-416
    [17]
    Bialy B J, Klotz J, Curtis J W, Dixon W E. An adaptive backstepping controller for a hypersonic air-breathing missile. In:Proceedings of the 2012 AIAA Guidance, Navigation and Control Conference. Minneapolis, MN:AIAA, 2012. AIAA-2012-4468
    [18]
    David O S, Pete J, Andrea S. Robust linear output feedback control of an airbreathing hypersonic vehicle. Journal of Guidance, Control, and Dynamics, 2008, 31(4):1052-1066
    [19]
    Zhang X, Lin Y. Adaptive output feedback tracking for a class of nonlinear systems. Automatica, 2012, 48(9):2372-2376
    [20]
    Fan H J, Han L X., Wen C Y, Xu L. Decentralized adaptive outputfeedback controller design for stochastic nonlinear interconnected systems. Automatica, 2012, 48(11):2866-2873
    [21]
    Jiang Zhong-Ping, Huang Jie. Stabilization and output regulation by nonlinear feedback:a brief overview. Acta Automatica Sinica, 2013, 39(9):1389-1401(in Chinese)
    [22]
    Tong S C, Li Y M, Feng G, Li T S. Observer-based adaptive fuzzy backstepping dynamic surface control for a class of MIMO nonlinear systems. IEEE Transactions on Systems, Man, and Cybernetics-Part B:Cybernetics, 2011, 41(12):1124-1135
    [23]
    Parker J T, Serrani A, Yurkovich S, Bolender M A, Doman D B. Controloriented modeling of an air-breathing hypersonic vehicle. Journal of Guidance, Control, and Dynamics, 2007, 30(3):856-869
    [24]
    Fiorentini L. Nonlinear Adaptive Controller Design for Air-Breathing Hypersonic Vehicles[Ph. D. dissertation], The Ohio State University, USA, 2010.
    [25]
    Tong S C, Li Y M, Feng G, Li T S. Observer-based adaptive fuzzy backstepping dynamic surface control for a class of non-linear systems with unknown time delays. IET Control Theory and Applications, 2011, 12(5):1426-1438
    [26]
    Han J Q. From PID to active disturbance rejection control. IEEE Transactions on Industrial Electronics, 2009, 56(3):900-906
    [27]
    Xia Y Q, Zhu Z, Fu M Y, Wang S. Attitude tracking of rigid spacecraft with bounded disturbances. IEEE Transactions on Industrial Electronics, 2011, 58(2):647-659
    [28]
    Chen M, Ge S S, Ren B B. Adaptive tracking control of uncertain MIMO nonlinear systems with input constraints. Automatica, 2011, 47(3):452-465
    [29]
    Sun H F, Yang Z L, Zeng J P. New tracking-control strategy for airbreathing hypersonic vehicles. Journal of Guidance, Control, and Dynamics, 2013, 36(3):846-859
    [30]
    Jiang Z P, Teel A R, Praly L. Small-gain theorem for ISS systems and application. Mathematics of Control, Signals, and Systems, 1994, 7(2):95-120

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (1086) PDF downloads(6) Cited by()

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return