2.765

2022影响因子

(CJCR)

  • 中文核心
  • EI
  • 中国科技核心
  • Scopus
  • CSCD
  • 英国科学文摘

留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

航天器姿态受限的协同势函数族设计方法

岳程斐 霍涛 陈雪芹 沈强 曹喜滨

岳程斐, 霍涛, 陈雪芹, 沈强, 曹喜滨. 航天器姿态受限的协同势函数族设计方法. 自动化学报, 2024, 50(1): 54−65 doi: 10.16383/j.aas.c230409
引用本文: 岳程斐, 霍涛, 陈雪芹, 沈强, 曹喜滨. 航天器姿态受限的协同势函数族设计方法. 自动化学报, 2024, 50(1): 54−65 doi: 10.16383/j.aas.c230409
Yue Cheng-Fei, Huo Tao, Chen Xue-Qin, Shen Qiang, Cao Xi-Bin. Synergistic potential functions for constrained attitude control of rigid spacecraft. Acta Automatica Sinica, 2024, 50(1): 54−65 doi: 10.16383/j.aas.c230409
Citation: Yue Cheng-Fei, Huo Tao, Chen Xue-Qin, Shen Qiang, Cao Xi-Bin. Synergistic potential functions for constrained attitude control of rigid spacecraft. Acta Automatica Sinica, 2024, 50(1): 54−65 doi: 10.16383/j.aas.c230409

航天器姿态受限的协同势函数族设计方法

doi: 10.16383/j.aas.c230409
基金项目: 国家自然科学基金(62003115, 11972130)资助
详细信息
    作者简介:

    岳程斐:哈尔滨工业大学(深圳)空间科学与应用技术研究院副教授. 主要研究方向为航天器高性能控制与在轨服务. 本文通信作者. E-mail: yuechengfei@hit.edu.cn

    霍涛:哈尔滨工业大学卫星技术研究所博士研究生. 主要研究方向为航天器姿态控制. E-mail: 22B918089@stu.hit.edu.cn

    陈雪芹:哈尔滨工业大学卫星技术研究所研究员. 主要研究方向为故障诊断, 容错控制. E-mail: cxqhit@163.com

    沈强:上海交通大学航空航天学院副教授. 主要研究方向为容错控制, 编队控制. E-mail: qiangshen@sjtu.edu.cn

    曹喜滨:中国工程院院士. 主要研究方向为卫星总体设计与仿真. E-mail: xbcao@hit.edu.cn

Synergistic Potential Functions for Constrained Attitude Control of Rigid Spacecraft

Funds: Supported by National Natural Science Foundation of China (62003115, 11972130)
More Information
    Author Bio:

    YUE Cheng-Fei Associate professor at the Institute of Space Science and Applied Technology, Harbin Institute of Technology (Shenzhen). His research interest covers high performance control of spacecraft and on-orbit service. Corresponding author of this paper

    HUO Tao Ph.D. candidate at the Research Center of Satellite Technology, Harbin Institute of Technology. His main research interest is spacecraft attitude control

    CHEN Xue-Qin Professor at the Research Center of Satellite Technology, Harbin Institute of Technology. Her research interest covers fault diagnosis and fault-tolerant control

    SHEN Qiang Associate professor at the School of Aeronautics and Astronautics, Shanghai Jiao Tong University. His research interest covers fault-tolerant control and formation control

    CAO Xi-Bin Academician of Chinese Academy of Engineering. His research interest covers system design and simulation of satellites

  • 摘要: 提出一种考虑航天器姿态约束的协同势函数设计方法, 在姿态全局收敛的同时, 保证姿态在机动过程中始终满足姿态约束. 首先, 建立航天器姿态指向约束模型, 并针对每一个指向约束设计软约束区域; 然后, 基于“角度扰动”方法设计协同势函数族; 接着, 通过设计协同势函数族内函数切换规律, 在软约束区域内构建满足姿态约束的势函数, 并给出区域内势函数临界点分布的调整方法; 最后, 将所得的势函数用于航天器的避障控制, 以比例−微分控制为例, 通过数值仿真, 验证该方法的有效性.
  • 图  1  姿态限制示意图

    Fig.  1  Illustration of attitude constraint

    图  2  使用协同势函数族的姿态控制示意图

    Fig.  2  Illustration of attitude control by means of synergistic potential functions

    图  3  $k{P_{{{{\boldsymbol{A}}}}}}\left( {\boldsymbol{R}} \right)$取值范围随$\Phi_{{{\boldsymbol R}}}$的变化曲线

    Fig.  3  The change curve of the range of$k{P_{{{{\boldsymbol{A}}}}}}\left( {\boldsymbol{R}} \right)$with$\Phi_{{{\boldsymbol R}}}$

    图  4  引理5的图示

    Fig.  4  Illustration of lemma 5

    图  5  无切换下姿态机动仿真

    Fig.  5  Attitude maneuver simulation without switching

    图  6  避障切换下姿态机动仿真

    Fig.  6  Attitude maneuver simulation when avoiding attitude constraints

    图  7  临界点切换下姿态机动仿真

    Fig.  7  Attitude maneuver simulation when avoiding critical points

    表  1  惯性系下姿态限制

    Table  1  Attitude constraints in the inertial frame

    序号 指向${\boldsymbol{v}}$ 角度$\alpha \ (^ \circ) $
    CZ1 $\left[ {0.5237,0.7208,0.4540} \right]^{\rm{T}}$ 20
    CZ2 $\left[ {-0.5530,0.7612,-0.3387} \right]^{\rm{T}}$ 15
    CZ3 $\left[ {-0.1488,-0.9393,0.3090} \right]^{\rm{T}}$ 25
    下载: 导出CSV
  • [1] 马亚杰, 姜斌, 任好. 航天器位姿运动一体化直接自适应容错控制研究. 自动化学报, 2023, 49(3): 678-686

    Ma Ya-Jie, Jiang Bin, Ren Hao. Adaptive direct fault-tolerant control design for spacecraft integrated attitude and orbit system. Acta Automatica Sinica, 2023, 49(3): 678-686
    [2] 钱辰, 方勇纯, 李友朋. 面向扑翼飞行控制的建模与奇异摄动分析. 自动化学报, 2022, 48(2): 434-443

    Qian Chen, Fang Yong-Chun, Li You-Peng. Control oriented modeling and singular perturbation analysis in flapping-wing flight. Acta Automatica Sinica, 2022, 48(2): 434-443
    [3] Bhat S P, Bernstein D S. A topological obstruction to continuous global stabilization of rotational motion and the unwinding phenomenon. Systems & Control Letters, 2000, 39(1): 63-70
    [4] Sanyal A, Fosbury A, Chaturvedi N, Bernstein D S. Inertia-free spacecraft attitude tracking with disturbance rejection and almost global stabilization. Journal of Guidance, Control, and Dynamics, 2009, 32(4): 1167-1178 doi: 10.2514/1.41565
    [5] 郑重, 李鹏, 钱默抒. 具有角速度和输入约束的航天器姿态协同控制. 自动化学报, 2021, 47(6): 1444-1452

    Zheng Zhong, Li Peng, Qian Mo-Shu. Spacecraft attitude coordination control with angular velocity and input constraints. Acta Automatica Sinica, 2021, 47(6): 1444-1452
    [6] Wang W, Tayebi A. Hybrid feedback for global tracking on matrix Lie groups SO(3) and SE(3). IEEE Transactions on Automatic Control, 2022, 67(6): 2930-2945 doi: 10.1109/TAC.2021.3097704
    [7] Hashemi S H, Pariz N, Sani S K H. Observer-based adaptive hybrid feedback for robust global attitude stabilization of a rigid body. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57(3): 1919-1929 doi: 10.1109/TAES.2021.3050665
    [8] Mayhew C G, Teel A R. Synergistic potential functions for hybrid control of rigid-body attitude. In: Proceedings of the American Control Conference. San Francisco, USA: IEEE, 2011. 875− 880
    [9] Casau P, Sanfelice R G, Cunha R, Silvestre C. A globally asymptotically stabilizing trajectory tracking controller for fully actuated rigid bodies using landmark-based information. International Journal of Robust and Nonlinear Control, 2015, 25(18): 3617-3640 doi: 10.1002/rnc.3283
    [10] Berkane S, Tayebi A. Construction of synergistic potential functions on SO(3) with application to velocity-free hybrid attitude stabilization. IEEE Transactions on Automatic Control, 2017, 62(1): 495-501 doi: 10.1109/TAC.2016.2560537
    [11] Lee T. Global exponential attitude tracking controls on SO(3). IEEE Transactions on Automatic Control, 2015, 60(10): 2837-2842 doi: 10.1109/TAC.2015.2407452
    [12] 胡庆雷, 邵小东, 杨昊旸, 段超. 航天器多约束姿态规划与控制:进展与展望. 航空学报, 2022, 43(10): 22.527351

    Hu Qing-Lei, Shao Xiao-Dong, Yang Hao-Yang, Duan Chao. Spacecraft attitude planning and control under multiple constraints: Review and prospects. Acta Aeronautica et Astronautica Sinica, 2022, 43(10): 22.527351
    [13] Shen Q, Yue C, Goh C H, Wu B, Wang D. Rigid-body attitude stabilization with attitude and angular rate constraints. Automatica, 2018, 90: 157-163 doi: 10.1016/j.automatica.2017.12.029
    [14] Tan X, Berkane S, Dimarogonas D V. Constrained attitude maneuvers on SO(3): rotation space sampling, planning and low-level control. Automatica, DOI: 10.1016/j.automatica.2019.108659
    [15] Yue C, Huo T, Lu M, Shen Q, Li C, Chen X, Cao X. A systematic method for constrained attitude control under input saturation. IEEE Transactions on Aerospace and Electronic Systems, 2023: 1-12, Doi: 10.1109/TAES.2023.3268607, to be published
    [16] Tian Y, Hu Q, Shao X. Adaptive fault-tolerant control for attitude reorientation under complex attitude constraints. Aerospace Science and Technology, Doi: 10.1109/TAES.2014.120240
    [17] Du Q H. Metrics for 3d rotations: comparison and analysis. Journal of Mathematical Imaging & Vision, 2009, 35(2): 155-164
    [18] Murray R M, Li Z, Shankar S S. A Mathematical Introduction to Robotic Manipulation. Boca Raton: CRC Press, 1994. 29−30
    [19] Berkane S, Abdessameud A, Tayebi A. On the design of globally exponentially stable hybrid attitude and gyro-bias observers [Online], available: https://arxiv.org/abs/1605.05640, May 9, 2023
    [20] Iwase N, Mimura M, Nishimoto T. Lusternik-schnirelmann category of non-simply connected compact simple lie groups. Topology and its Applications, 2005, 150(1): 111-123
    [21] Chen T and Shan J. Continuous constrained attitude regulation of multiple spacecraft on SO(3). Aerospace Science and Technology, Doi: 10.1016/j.ast.2020.105769
    [22] Hu Q, Chi B, Akella M R. Anti-unwinding attitude control of spacecraft with forbidden pointing constraints. Journal of Guidance, Control, and Dynamics, 2019, 42(4): 822-835 doi: 10.2514/1.G003606
    [23] Mayhew C G, Teel A R. Hybrid control of rigid-body attitude with synergistic potential functions. In: Proceedings of the American Control Conference. San Francisco, USA: IEEE, 2011. 287−292
    [24] Kulumani S, Lee T. Constrained geometric attitude control on SO(3). International Journal of Control, Automation and Systems, 2017, 15(6): 2796-2809 doi: 10.1007/s12555-016-0607-4
  • 加载中
图(7) / 表(1)
计量
  • 文章访问数:  381
  • HTML全文浏览量:  207
  • PDF下载量:  137
  • 被引次数: 0
出版历程
  • 收稿日期:  2023-07-04
  • 录用日期:  2023-09-26
  • 网络出版日期:  2023-12-05
  • 刊出日期:  2024-01-29

目录

    /

    返回文章
    返回