YI Zhong-gui, GE Xin-sheng. Optimal Attitude Control of Underactuated Spacecrafts With the Gauss Pseudospectral Method[J]. Applied Mathematics and Mechanics, 2017, 38(12): 1319-1330. doi: 10.21656/1000-0887.380013
Citation: YI Zhong-gui, GE Xin-sheng. Optimal Attitude Control of Underactuated Spacecrafts With the Gauss Pseudospectral Method[J]. Applied Mathematics and Mechanics, 2017, 38(12): 1319-1330. doi: 10.21656/1000-0887.380013

Optimal Attitude Control of Underactuated Spacecrafts With the Gauss Pseudospectral Method

doi: 10.21656/1000-0887.380013
Funds:  The National Natural Science Foundation of China(11472058)
  • Received Date: 2017-01-10
  • Rev Recd Date: 2017-02-20
  • Publish Date: 2017-12-15
  • The attitude and orientation of modern spacecrafts generally can be controlled by 3 orthogonal reaction momentum wheels. The attitude control of underactuated spacecrafts with only 2 momentum wheels and failed out of complete 3-axis controlling torques, was investigated. The control problem was converted to a nonholonomic motion planning problem of a drift-free system with zero angular momentum. The attitude motion planning problem of a spacecraft with 2 momentum wheels was converted to a nonlinear programming problem (NLP) with the Gauss pseudospectral method, and then solved with the SQP algorithm. Through numerical simulation the optimal control met the design requirements of zero boundaries, so the wheels can be controlled easily by servomotors; the planned attitude curves were almost identical to the numerically integrated solutions; the number of suitable collocation points was found through balancing among 3 factors: the target function value, the running time and the solution error. The results show that the proposed method is effective for the optimal attitude control of underactuated spacecrafts.
  • loading
  • [1]
    Crouch P E. Spacecraft attitude control and stabilization:applications of geometric control theory to rigid body models[J]. IEEE Transactions on Automatic Control,1984,29(4): 321-331.
    [2]
    Krishnan H, McClamroch N H, Reyhanoglu M. Attitude stabilization of a rigid spacecraft using two momentum wheel actuators[J]. Journal of Guidance Control & Dynamics,1995,18(2): 256-263.
    [3]
    Tsiotras P, Corless M, Longuski J M. A novel approach to the attitude control of axisymmetric spacecraft[J].Automatica,1995,31(8): 1099-1112.
    [4]
    Krishnaprasad P S. Geometric phases, and optimal reconfiguration for multibody systems[C]// Proceedings of the American Control Conference. New York: The American Automatic Control Council, 1990: 2440-2444.
    [5]
    Walsh G C, Montgomery R, Sastry S S. Orientation control of the dynamic satellite[C]// Proceedings of the American Control Conference. Baltimore, Maryland: The American Automatic Control Council, 1994: 138-142.
    [6]
    Coverstone-Carroll V L, Wilkey N M. Optimal control of a satellite-robot system using direct collocation with nonlinear programming[J]. Acta Astronautica,1995,36(3): 149-162.
    [7]
    戈新生, 陈立群, 刘延柱. 带有两个动量飞轮刚体航天器的姿态非完整运动规划问题[J]. 控制理论与应用, 2004,21(5): 781-784.(GE Xin-sheng, CHEN Li-qun, LIU Yan-zhu. Nonholonomic motion planning for the attitude of rigid spacecraft with two momentum wheel actuators[J]. Control Theory & Applications,2004,21(5): 781-784.(in Chinese))
    [8]
    孙凯, 戈新生. 航天器太阳帆板伸展过程最优控制的粒子群优化算法[J]. 工程力学, 2007,24(9): 188-192.(SUN Kai, GE Xin-sheng. Optimal control of stretching process of solar array on spacecraft using particle swarm optimization algorithm[J]. Engineering Mechanics,2007,24(9): 188-192.(in Chinese))
    [9]
    段柳成, 李海泉, 刘晓峰, 等. 考虑铰摩擦的太阳翼展开动力学研究[J]. 应用数学和力学, 2014,35(12): 1308-1319.(DUAN Liu-cheng, LI Hai-quan, LIU Xiao-feng, et al. Deployment dynamics for solar wings with joint friction[J]. Applied Mathematics and Mechanics,2014,35(12): 1308-1319.(in Chinese))
    [10]
    Benson D A, Huntington G T, Thorvaldsen T P, et al. Direct trajectory optimization and costate estimation via an orthogonal collocation method[J]. Journal of Guidance, Control, and Dynamics,2006,29(6): 1435-1440.
    [11]
    Benson D. A Gauss pseudospectral transcription for optimal control[D]. PhD Thesis. Cambridge, Massachusetts: Massachusetts Institute of Technology, 2005.
    [12]
    雍恩米, 唐国金, 陈磊. 基于Gauss伪谱方法的高超声速飞行器再入轨迹快速优化[J]. 宇航学报, 2008,29(6): 1766-1772.(YONG En-mi, TANG Guo-jin, CHEN Lei. Rapid trajectory optimization for hypersonic reentry vehicle via Gauss pseudospectral method[J]. Journal of Astronautics,2008,29(6): 1766-1772.(in Chinese))
    [13]
    李适. 空间机器人路径优化与鲁棒跟踪控制[D]. 博士学位论文. 哈尔滨: 哈尔滨工业大学, 2013.(LI Shi. Path optimization and robust tracking control for space manipulator[D]. PhD Thesis. Harbin: Harbin Institute of Technology, 2013.(in Chinese))
    [14]
    董雪仰, 戈新生. 航天器太阳帆板展开过程最优控制的自适应Gauss伪谱法[J]. 应用数学和力学, 2016,37(6): 655-664.(DONG Xue-yang, GE Xin-sheng. The adaptive Gauss pseudospectral method for the optimal control of spacecraft solar array deployment[J]. Applied Mathematics and Mechanics,2016,37(6): 655-664.(in Chinese))
    [15]
    易中贵, 戈新生. 自由下落猫姿态最优控制的混合优化策略[J]. 力学学报, 2016,48(6): 1390-1397.(YI Zhong-gui, GE Xin-sheng. The attitude optimal control with a hybrid optimal strategy for a free-falling cat[J]. Chinese Journal of Theoretical and Applied Mechanics,2016,48(6): 1390-1397.(in Chinese))
    [16]
    庄宇飞, 马广富, 黄海滨. 欠驱动刚性航天器时间最优轨迹规划设计[J]. 控制与决策, 2010,25(10): 1469-1473.(ZHUANG Yu-fei, MA Guang-fu, HUANG Hai-bin. Time-optimal motion planning of an underactuated rigid spacecraft[J]. Control and Decision,2010,25(10): 1469-1473.(in Chinese))
    [17]
    ZHUANG Yu-fei, MA Guang-fu, LI Chuan-jiang, et al. Time-optimal trajectory planning of underactuated rigid spacecraft using differential flatness[J]. Journal of Astronautics,2011,32(8): 1753-1761.
    [18]
    吴锦杰, 刘昆, 韩大鹏, 等. 欠驱动航天器相对运动的姿轨耦合控制[J]. 控制与决策, 2014,29(6): 969-978.(WU Jin-jie, LIU Kun, HAN Da-peng, et al. Coupled attitude and orbit control for relative motion of underactuated spacecraft[J]. Control and Decision,2014,29(6): 969-978.(in Chinese))
    [19]
    刘延柱, 潘振宽, 戈新生. 多体系统动力学[M]. 2版. 北京: 高等教育出版社, 2014.(LIU Yan-zhu, PAN Zhen-kuan, GE Xin-sheng. Dynamics of Multibody Systems [M]. 2nd ed. BeiJing: Higher Education Press, 2014.(in Chinese))
    [20]
    刘延柱. 航天器姿态动力学[M]. 北京: 国防工业出版社, 1995.(LIU Yan-zhu. Spacecraft Attitude Dynamics [M]. Beijing: National Defense Industry Press, 1995.(in Chinese))
  • 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

    Article Metrics

    Article views (1132) PDF downloads(549) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return