Volume 40 Issue 3
May  2020
Turn off MathJax
Article Contents
WANG Hongwei, SONG Xiaojuan, LI Changjie. Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft[J]. Journal of Space Science, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408
Citation: WANG Hongwei, SONG Xiaojuan, LI Changjie. Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft[J]. Journal of Space Science, 2020, 40(3): 408-418. doi: 10.11728/cjss2020.03.408

Adaptive Passive Control for Large-angle Attitude Maneuver of Liquid-filled Spacecraft

doi: 10.11728/cjss2020.03.408
  • Received Date: 2019-03-06
  • Rev Recd Date: 2020-02-11
  • Publish Date: 2020-05-15
  • In this paper, the large-angle attitude maneuver of three-axis stabilized liquid-filled spacecraft based on adaptive passive control is studied. The liquid sloshing is equivalent to the viscous spherical pendulum model, and the dynamic model of the coupled system is established by using the law of conservation of angular momentum. In view of the fact that gyroscope faults or gyroscope-free configuration lead to no angular velocity measurement of spacecraft attitude, considering the characteristics of unknown external disturbance, the moment of inertia uncertainty and the un-measurable characteristics of liquid sloshing displacement, the adaptive output feedback passive control law is designed for large angel attitude maneuver of spacecraft. The adaptive update laws are used to compensate for external disturbances and estimate state variables for liquid sloshing. The Lyapunov method and LaSalle invariant lemma prove that the control law can not only ensure the asymptotic stability of the closed-loop system but also ensure the two desired equilibrium positions are stable. Finally, simulation results verify the effectiveness of the proposed control method.


  • loading
  • [1]
    YUE Baozeng, SONG Xiaojuan. Advance in rigid-flexible-liquid-control coupling dynamics of spacecraft[J]. Adv. Mech., 2013, 43(1):163-173(岳宝增, 宋晓娟. 具有刚-柔-液-控耦合的航天器动力学研究进展[J]. 力学进展, 2013, 43(1):163-173)
    YUE B, WU W, YAN Y. Modeling and coupling dynamics of the spacecraft with multiple propellant tanks[J]. AIAA J., 2016, 54(11):1-11
    DENG Mingle, YUE Baozeng, HUANG hua. Study on equivalent mechanical model of large-scale liquid sloshing[J]. J. Astron., 2016, 37(6):631-638(邓明乐, 岳宝增, 黄华. 液体大幅晃动类等效力学模型研究[J]. 宇航学报. 2016, 37(6):631-638)
    LI Qing, MA Xingrui, WANG Tianshu. Equivalent mechanical model for liquid sloshing in non-axisymmetric tanks[J]. J. Astron., 2011, 32(2):242-249(李青, 马兴瑞, 王天舒. 非轴对称贮箱液体晃动的等效力学模型[J]. 宇航学报, 2011, 32(2):242-249)
    SONG Xiaojuan, YUE Baozeng, YAN Yulong, et al. Hybrid attitude maneuver control of liquid multi-mode sloshing liquid-filled spacecraft[J]. J. Astron., 2015, 36(7):819-825(宋晓娟, 岳宝增, 闫玉龙, 等. 液体多模态晃动充液航天器姿态机动复合控制[J]. 宇航学报, 2015, 36(7):819-825)
    YUE B Z. Heteroclinic bifurcations in completely liquid-filled spacecraft with flexible appendage[J]. Nonlin. Dynam., 2007, 51(1):317-327
    YUE B Z. Study on the chaotic dynamics in attitude maneuver of liquid-filled flexible spacecraft[J]. AIAA J., 2011, 49(10):2090-2099
    REYHANOGLU M, HERVAS J R. Nonlinear control of space vehicles with multi-mass fuel slosh dynamics[C]//International Conference on Recent Advances in Space Technologies. Piscataway:IEEE Press, 2011:247-252
    REYHANOGLU M, HERVAS J R. Nonlinear dynamics and control of space vehicles with multiple fuel slosh modes[J]. Control Eng. Pract., 2012, 20(9):912-918
    KANG J Y, LEE S. Attitude acquisition of a satellite with a partially filled liquid tank[J]. J. Guid. Control Dyn., 2012, 31(3):790-793
    KANG J Y, COCHRAN J. Resonant motion of a spin-stabilized thrusting spacecraft[J]. J. Guid. Control Dyn., 2004, 27(3):356-365
    DU Hui. Attitude control of passive lunar lander with liquid sloshing[J]. Space Control Technol. Appl., 2011, 37(1):50-54(杜辉. 基于无源性的带液体晃动月球着陆器的姿态控制[J]. 空间控制技术与应用, 2011, 37(1):50-54)
    CAI Jian, WANG Fang, ZHANG Honghua. Attitude tracking control of flexible spacecraft based on passivity[J]. J. Astron., 2010, 31(4):1030-1035(蔡建, 王芳, 张洪华. 基于无源性的挠性航天器姿态跟踪控制[J]. 宇航学报, 2010, 31(4):1030-1035)
    LIZARRALDE, WEN J T. Attitude control without angular velocity measurement:a passivity approach[C]//IEEE International Conference on Robotics and Automation, 1995 Proceedings. Nagoya:IEEE, 1995.DOI:10. 1109/ROBOT.1995.525665
    TSIOTRAS P. A passivity approach to attitude stabilization using nonredundant kinematic parameterizations[C]//Proceedings of the 34th Conference on Decision and Control, 1995.DOI: 10.1109/CDC.1995.478944
    COSTIC B T, DAWSON D M, DE QUEIROZ M, et al. A quaternion-based adaptive attitude tracking controller without velocity measurements[J]. J. Guid. Control Dyn., 2001, 24(6):1214-1222
    DI GENNARO S. Attitude tracking for flexible spacecraft from quaternion measurements[C]//Proceedings of the 41st IEEE Conference on Decision and Control. Las Vegas:IEEE, 2002:4090-4091
    GENNARO S D. Passive attitude control of flexible spacecraft from quaternion measurements[J]. J. Optim. Theory Appl., 2003, 116(1):41-60
    YIN Chunwu, HOU Mingshan, LI Mingxiang. Attitude tracking dynamic PD control without angular velocity measurement[J]. J. Motor. Control, 2017, 21(12):107-116(殷春武, 侯明善, 李明翔. 无角速度测量的姿态跟踪动态PD控制[J]. 电机与控制学报, 2017, 21(12):107-116)
    ZHU Qiao, WANG Xudong, CUI Jiarui. Quaternion-based spacecraft attitude nonlinear controller[J]. Inf. Cont., 2012, 41(2):170-173(祝乔, 汪旭东, 崔家瑞. 基于四元数的航天器姿态非线性控制器[J]. 信息与控制, 2012, 41(2):170-173)
    SHI Xingyu, QI Ruiyun. Modeling and attitude stability control of three-axis liquid-filled spacecraft[J]. J. Nanjing Univ. Aeron. Astron., 2017, 49(1):132-139(史星宇, 齐瑞云. 三轴充液航天器建模及姿态稳定控制[J]. 南京航空航天大学学报, 2017, 49(1):132-139)
    LIU F, YUE B, ZHAO L. Attitude dynamics and control of spacecraft with a partially filled liquid tank and flexible panels[J]. Acta Astron., 2018, 143:327-336
    ISIDORI A. Nonlinear Control Systems[M]. New York:Springer Science and Business Media, 2013
  • 加载中


    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(417) PDF Downloads(39) Cited by()
    Proportional views


    DownLoad:  Full-Size Img  PowerPoint