Volume 36 Issue 10
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LEI Hao, CHEN Boyi, LIU Yanbin, LU Yuping. Longitudinal attitude control for very flexible aircraft with thrust cooperation[J]. Journal of Aerospace Power, 2021, 36(10): 2207-2217. doi: 10.13224/j.cnki.jasp.20200457
Citation: LEI Hao, CHEN Boyi, LIU Yanbin, LU Yuping. Longitudinal attitude control for very flexible aircraft with thrust cooperation[J]. Journal of Aerospace Power, 2021, 36(10): 2207-2217. doi: 10.13224/j.cnki.jasp.20200457
shu

Longitudinal attitude control for very flexible aircraft with thrust cooperation

doi: 10.13224/j.cnki.jasp.20200457
  • 1.

    College of Automation Engineering，Nanjing University of Aeronautics and Astronautics，Nanjing 211106，China

  • 2.

    College of Astronautics，Nanjing University of Aeronautics and Astronautics，Nanjing 211106，China

  • Received Date: 2020-10-29
  • Publish Date: 2021-10-28
    Abstract
  • The improved multi-body model of very flexible aircraft was proposed to analyse the flight/structure coupled dynamics characteristics of very flexible aircraft,the longitudinal dynamics characteristics of very flexible aircraft were studied and the longitudinal attitude controller was designed.The dynamics of dihedral angle was used to approximate the structural dynamics characteristics of very flexible aircraft,and the coupled longitudinal dynamics model was derived.The improved model was trimmed under different load conditions,and the relationship between the stability and deformation of the system was analyzed according to the linearized model at the equilibrium point.The longitudinal attitude controller was designed for attitude stabilization and tracking of very flexible aircraft.Compared with conventional aircrafts,large deformation occurs during the flight of very flexible aircraft.When the load was large,the trimmed configuration was approximately “U” shaped,and the longitudinal phugoid period was unstable.The results showed that as the deformation increased,the coupling between the modes increased.The longitudinal attitude control of very flexible aircraft needed to control the velocity at the same time and takes the coupled structure dynamics into account,otherwise,due to the coupling effect between structure and flight dynamics,the system will even be divergent.

     

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    • References(22)
  • [1]
    张健，张德虎.高空长航时太阳能无人机总体设计要点分析[J].航空学报，2016，37（增刊1）:S1-S7.
    [2]
    GIBSON T，ANNASWAMY A，LAVRETSKY E.Modeling for control of very flexible aircraft[R].AIAA 2011-6202,2011.
    [3]
    NOLL T E，BROWN J M，PEREZ-DAVIS M E，et al.Investigation of the helios prototype aircraft mishap：Volume Ⅰ mishap report[R].NASA Report 64317，2004.
    [4]
    王伟.太阳能无人机非线性气动弹性及飞行力学研究[D].西安：西北工业大学，2015.
    [5]
    PATIL M J，HODGES D H.Flight dynamics of highly flexible flying wings[J].Journal of Aircraft，2006，43（6）:1790-1798.
    [6]
    CHANG C S，HODGES D H，PATIL M J.Flight dynamics of highly flexible aircraft[J].Journal of Aircraft，2008，45（2）:538-545.
    [7]
    RAGHAVAN B，PATIL M J.Flight dynamics of high aspect-ratio flying wings:effect of large trim deformation[J].Journal of Aircraft，2009，46（5）:1808-1812.
    [8]
    SU W，CESNIK C E S.Dynamic response of highly flexible flying wings[J].AIAA Journal，2011，49（2）:324-339.
    [9]
    CESNIK C E S，SU W.Nonlinear aeroelastic modeling and analysis of fully flexible aircraft[R].AIAA-2005-2169，2005.
    [10]
    SU W，CESNIK C E S.Strain-based geometrically nonlinear beam formulation for modeling very flexible aircraft[J].International Journal of Solids and Structures，2011，48（16/17）:2349-2360.
    [11]
    O'ROURKE I，KOLMANOVSKY I，GARONE E，et al.Explicit reference governor for constrained maneuver and shape control of a seven-state multibody aircraft[R].AIAA 2020-1830，2020.
    [12]
    张勇，陆宇平，刘燕斌，等.高超声速飞行器控制一体化设计[J].航空动力学报，2012，27（12）:2724-2732.
    [13]
    肖地波，陆宇平，姚克明，等.高超声速飞行器推进系统建模[J].航空动力学报，2015，30（4）:944-951.
    [14]
    张勇.面向控制的高超声速飞行器一体化设计[D].南京：南京航空航天大学，2011.
    [15]
    AFONSO F，VALE J，OLIVEIRA E，et al.A review on non-linear aeroelasticity of high aspect-ratio wings[J].Progress in Aerospace Sciences，2017，89:40-57.
    [16]
    曾惠华，刘钟坤.大展弦比机翼几何非线性颤振风洞试验研究[J].装备环境工程，2019，16（1）:68-72.
    [17]
    向锦武，张雪娇，赵仕伟，等.大展弦比复合材料机翼研究进展[J].哈尔滨工业大学学报，2017，49（10）:1-14.
    [18]
    PATIL M J，HODGES D H，CESNIK C E S.Characterizing the effects of geometrical nonlinearities on aeroelastic behavior of high-aspect-ratio wings[C]∥Proceedings of International Forum on Aeroelasticity and Structural Dynamics.Williamsburg，Virginia，US：NASA,1999:1-10.
    [19]
    RAGHAVAN B.Flight dynamics and control of highly flexible flying-wings[D].Blacksburg，US:Virginia Polytechnic Institute and State University，2009.
    [20]
    王子安，龚正，陈永亮，等.复合翼无人机加速段纵向飞行特性分析与控制设计[J].航空动力学报，2019，34（10）:2177-2190.
    [21]
    SKOGESTAD S，POSTLETHWAITE I.Multivariable feedback control:analysis and design[M].Chichester，UK:John Wiley & Sons Inc，1996.
    [22]
    吴森堂.飞行控制系统[M].北京：北京航空航天大学出版社，2013.
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