Advanced Search
Volume 33 Issue 10
Oct.  2007
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2007  >  33(10): 1233-1236.
Chen Lei, Chen Zongji. Vision-based autonomous landing integrated navigation scheme of unmanned combat aerial vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(02): 159-163. (in Chinese)
Citation: Zheng Minjie, Xu Shijie. Spacecraft attitude slew maneuver control via backstepping method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1233-1236. (in Chinese)
shu

Spacecraft attitude slew maneuver control via backstepping method

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 03 Nov 2006
  • Publish Date: 31 Oct 2007
    Abstract
  • The backstepping control method was applied to the slew maneuver of the rigid spacecraft. In order to avoid the complicated calculation of the derivation of the intermediate control law which is required in the conventional backstepping method, the intermediate control law presents in a form of differential equation. On this basis, two methods were applied to reduce the requirement in the max actuator output torque by means of postponing the peak of the control torque. One method is to change the initialization of the intermediate control law. The other is to utilize a worse angular velocity tracking law. The system stability with the second control law depends on the parameters of the controller, however, the max control torque can be accurately restricted. Simulation results illuminate the availability of the derived control laws.

     

    • FullText(HTML)
    • References(1)
  • [1] Wie B, Bailey D, Heiberg C. Rapid multi-target acquisition and pointing control of agile spacecraft . AIAA-2000-4546, 2000 [2] Lappas V J, Steyn W H, Underwood C I. Practical results on the development of a control moment gyro based attitude control system for agile small satellites The Sixteenth Annual AIAA/USU Conference on Small Satellites. Logan, Utah: , 2002:12-15 [3] 汤亮,徐世杰.采用单框架控制力矩陀螺群的卫星侧摆机动控制研究[J].航天控制,2003,2: 1-5,13 Tang Liang, Xu Shijie. Skew maneuver control for satellites using SGCMG systems[J]. Aerospace Control, 2003,2: 1-5,13(in Chinese) [4] 徐世杰. 基于Lyapunov方法的空间飞行器大角度姿态机动控制[J]. 宇航学报, 2001,22(4):95-99 Xu Shijie. Large angle attitude maneuver control of spacecraft based on Lyapunov approach[J].Journal of Astronautics, 2001,22(4):95-99(in Chinese) [5] Kim K, Kim Y. Backstepping control of rigid spacecraft slew maneuver . AIAA-2001-4210, 2001 [6] Kim K, Kim Y. Robust backstepping control for slew maneuver using nonlinear tracking function IEEE Transactions on Control Systems Technology, 2003,11(6):822-829 [7] 肖业伦. 航空航天器运动的建模——飞行动力学的理论基础[M]. 北京:北京航空航天大学出版社,2003:128-138 Xiao Yelun. Modeling of aerostat and spacecraft: theories foundation of flight dynamics[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2003: 128-138 (in Chinese) [8] Hull R A, Ham C, Johnson R W. Systematic design of attitude control systems for a satellite in a circular orbit with guaranteed performance and stability Advanced Subsystems & Components, 2000:1-10
    • Relative Articles

  • Relative Articles

    [1]WANG Y J，CHEN Q Y，GAO X Z，et al. Guidance and control method for dynamic net-recovery of UAV and the flight test verification[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：487-497 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0043.
    [2]TAN C，YU P，LI B，et al. Pressure cascade control of brake-by-wire unit based on direct drive pump-valve cooperative[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（4）：1163-1171 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0216.
    [3]YIN W Z，LIAN D P，LI K Y，et al. Manipulator force/position hybrid control based on staged adaptation[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（1）：161-166 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0955.
    [4]WAN B，SU X C，WANG J，et al. A precise landing control method based on model predictive control algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（4）：1197-1207 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0383.
    [5]ZUO L，ZHANG X L，LI Z Y，et al. UAV control law design method based on active-disturbance rejection control[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1512-1522 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0488.
    [6]LIU S Y，YANG H L，ZHANG Z G，et al. Vibration control of flexible spacecraft with output constraints and external disturbances[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1560-1567 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0622.
    [7]ZHANG Y L，MA Z Z，SHI L，et al. Multi-agent coverage control based on communication connectivity maintenance constraints[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（2）：519-528 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0340.
    [8]GUAN Y Z，FENG M. Application of active disturbance rejection control in gyro motor steady speed control[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：234-242 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0209.
    [9]ZHANG Y，YU H，YANG X X，et al. Adaptive group formation tracking-containment control for UAV swarm[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：97-109 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0264.
    [10]LIU B，HAO X H，CAI X. Classification method of radio fuze target and interference signal based on power spectrum entropy[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（3）：913-919 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0355.
    [11]DU X，SUN Z D，XU C L，et al. Pinning control of AUV cluster under input delay and communication delay[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1474-1480 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0538.
    [12]XU K D，XU Z B，GUO X X，et al. Analysis of CDMA interference in large-scale satellite constellation[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（9）：2885-2892 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0741.
    [13]WANG C Y，YANG L M，LI Y H. A mapping leader formation control strategy for multiple mobile robots based on two-stage sliding mode control[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：3108-3114 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0792.
    [14]CHEN T T，WANG F Y，XIA C Y，et al. Tracking control of multi-agent systems based on persistent-hold mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3321-3327 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0065.
    [15]LI C，HE Y Z，HU Y. Characteristic model control of nutation target contact detumbling[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（11）：2977-2988 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0798.
    [16]XIA Xin-hui, JIA Ying-hong, ZHANG Jun. Spherical-caging-based control of a dual-arm space robot for capturing an object[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0258
    [17]LI J F，ZHAO D Q，WANG D M，et al. A quality evaluation method for wavelet denoising based on combinatorial weighting method[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：718-725 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0303.
    [18]HAN X L，SHANGGUAN H，ZHANG X，et al. A low-dose CT image denoising method based on artifact estimation[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（2）：491-502 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0263.
    [19]WANG Yingxun, SONG Xinyu, ZHAO Jiang, CAI Zhihao. Anti-disturbance trajectory tracking control method for aggressive quadrotors[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1806-1817. doi: 10.13700/j.bh.1001-5965.2022.0216
    [20]YIN Zengyuan, CAI Yuanwen, REN Yuan, WANG Weijie, CHEN Xiaocen, YU Chunmiao. Decoupled active disturbance rejection control method for magnetically suspended rotor based on state feedback[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1210-1221. doi: 10.13700/j.bh.1001-5965.2021.0021
    • Supplements(0)
    • Cited By
  • 加载中

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
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(3288) PDF downloads(834) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return