2.845

2023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

求解含复杂约束非线性最优控制问题的改进Gauss伪谱法

孙勇 张卯瑞 梁晓玲

孙勇, 张卯瑞, 梁晓玲. 求解含复杂约束非线性最优控制问题的改进Gauss伪谱法. 自动化学报, 2013, 39(5): 672-678. doi: 10.3724/SP.J.1004.2013.00672
引用本文: 孙勇, 张卯瑞, 梁晓玲. 求解含复杂约束非线性最优控制问题的改进Gauss伪谱法. 自动化学报, 2013, 39(5): 672-678. doi: 10.3724/SP.J.1004.2013.00672
SUN Yong, ZHANG Mao-Rui, LIANG Xiao-Ling. Improved Gauss Pseudospectral Method for Solving Nonlinear Optimal Control Problem with Complex Constraints. ACTA AUTOMATICA SINICA, 2013, 39(5): 672-678. doi: 10.3724/SP.J.1004.2013.00672
Citation: SUN Yong, ZHANG Mao-Rui, LIANG Xiao-Ling. Improved Gauss Pseudospectral Method for Solving Nonlinear Optimal Control Problem with Complex Constraints. ACTA AUTOMATICA SINICA, 2013, 39(5): 672-678. doi: 10.3724/SP.J.1004.2013.00672

求解含复杂约束非线性最优控制问题的改进Gauss伪谱法

doi: 10.3724/SP.J.1004.2013.00672
详细信息
    通讯作者:

    孙勇

Improved Gauss Pseudospectral Method for Solving Nonlinear Optimal Control Problem with Complex Constraints

  • 摘要: 针对含有复杂约束条件的非线性最优控制问题,提出了一种改进的Gauss伪谱法 (Improved Gauss pseudospectral method, IGPM). 这类问题难以得到解析解,特别是有些问题不存在解析的模型, 一些参数只能通过查表得到,使得传统方法难以求解. 在传统的Gauss伪谱法的基础上,将非线性的终端状态积分约束等价地转化为线性形式,提出了IGPM, 通过协态映射定理可以计算出协态变量,检验最优性,使得IGPM具有间接法一样的精度. 并且给出了初始时刻协态变量和端点时刻控制变量的计算方法. 为了提高解的精度,基于IGPM提出了迭代算法, 最后将该算法应用于求解高超声速飞行器上升段轨迹优化问题,结果表明最优轨迹基本满足路径约束条件和最优性条件.
  • [1] Betts J T. Survey of numerical methods for trajectory optimization. Journal of Guidance, Control, and Dynamics, 1998, 21(2): 193-207[2] Wei Q L, Zhang H G, Liu D R, Zhao Y. An optimal control scheme for a class of discrete-time nonlinear systems with time delays using adaptive dynamic programming. Acta Automatica Sinica, 2010, 36(1): 121-129[3] Kong S L, Zhang Z S. Optimal control of stochastic system with Markovian jumping and multiplicative noises. Acta Automatica Sinica, 2012, 38(7): 1113-1118[4] Li Jia-Feng, Zhou Hao, Chen Wan-Chun. Indirect method for the hypersonic vehicle maximum-glide problem. Flight Dynamics, 2009, 27(3): 41-44, 49 (李佳峰, 周浩, 陈万春. 高超声速飞行器滑行段最优弹道的间接算法. 飞行力学, 2009, 27(3): 41-44, 49)[5] Li Hui-Feng, Li Zhao-Ying. Indirect method of optimal ascent guidance for hypersonic vehicle. Journal of Astronautics, 2011, 32(2): 297-302 (李惠峰, 李昭莹. 高超声速飞行器上升段最优制导间接法研究. 宇航学报, 2011, 32(2): 297-302)[6] Hager W W. Runge-Kutta methods in optimal control and the transformed adjoint system. Numerische Mathematik, 2000, 87(2): 247-282[7] Conway B A, Larson K M. Collocation versus differential inclusion in direct optimization. Journal of Guidance, Control and Dynamics, 2000, 21(5): 780-785[8] Elnagar G, Kazemi M A, Razzaghi M. The pseudospectral Legendre method for discretizing optimal control problems. IEEE Transactions on Automatic Control, 1995, 40(10): 1793-1796[9] Peng Hai-Jun, Gao Qiang, Wu Zhi-Gang, Zhong Wan-Xie. A mixed variable variational method for optimal control problems with applications in aerospace control. Acta Automatica Sinica, 2011, 37(10): 1248-1255 (彭海军, 高强, 吴志刚, 钟万勰. 求解最优控制问题的混合变量变分方法及其航天控制应用. 自动化学报, 2011, 37(10): 1248-1255)[10] Fahroo F, Ross I M. Costate estimation by a Legendre pseudospectral method. Journal of Guidance, Control, and Dynamics, 2001, 24(2): 270-277[11] Benson D A, Huntington G T, Thorvaldsen T P, Rao A V. Direct trajectory optimization and costate estimation via an orthogonal collocation method. Journal of Guidance, Control, and Dynamics, 2006, 29(6): 1435-1440[12] Huntington G T, Rao A V. Optimal reconfiguration of spacecraft formations using the gauss pseudospectral method. Journal of Guidance, Control, and Dynamics, 2008, 31(3): 689-698[13] Sun Y, Zhang M R. Optimal reentry range trajectory of hypersonic vehicle by Gauss pseudospectral method. In: Proceedings of the 2nd International Conference on Intelligent Control and Information. Harbin, China: IEEE, 2011. 545-549[14] Sun Y, Zhang M R, Li H. New costate estimation of Gauss pseudospectral method for nonlinear optimal control problem. In: Proceedings of the 2011 International Workshop on Engineering Application Research. Hangzhou, China: IEIT, 2011. 31-36[15] Kameswaran S, Biegler L T. Convergence rates for direct transcription of optimal control problems using collocation at radau points. Computational Optimization and Applications, 2008, 41(1): 81-126[16] Garg D, Hager W W, Rao A V. Pseudospectral methods for solving infinite-horizon optimal control problems. Automatica, 2011, 47(4): 829-837[17] Lu P, Sun H S, Tsai B. Closed-loop endoatmospheric ascent guidance. Journal of Guidance, Control, and Dynamics, 2003, 26(2): 283-294[18] Lu P, Pan B F. Highly constrained optimal launch ascent guidance. Journal of Guidance, Control, and Dynamics, 2010, 33(2): 404-414
  • 加载中
计量
  • 文章访问数:  1950
  • HTML全文浏览量:  109
  • PDF下载量:  2518
  • 被引次数: 0
出版历程
  • 收稿日期:  2012-05-15
  • 修回日期:  2012-08-31
  • 刊出日期:  2013-05-20

目录

    /

    返回文章
    返回