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
[2]
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)
[3]
Hager W W. Runge-Kutta methods in optimal control and the transformed adjoint system. Numerische Mathematik, 2000, 87(2): 247-282
[4]
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
[5]
Fahroo F, Ross I M. Costate estimation by a Legendre pseudospectral method. Journal of Guidance, Control, and Dynamics, 2001, 24(2): 270-277
[6]
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
[7]
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
[8]
Lu P, Sun H S, Tsai B. Closed-loop endoatmospheric ascent guidance. Journal of Guidance, Control, and Dynamics, 2003, 26(2): 283-294
[9]
Betts J T. Survey of numerical methods for trajectory optimization. Journal of Guidance, Control, and Dynamics, 1998, 21(2): 193-207
[10]
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
[11]
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)
[12]
Conway B A, Larson K M. Collocation versus differential inclusion in direct optimization. Journal of Guidance, Control and Dynamics, 2000, 21(5): 780-785
[13]
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)
[14]
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
[15]
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
[16]
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
[17]
Garg D, Hager W W, Rao A V. Pseudospectral methods for solving infinite-horizon optimal control problems. Automatica, 2011, 47(4): 829-837
[18]
Lu P, Pan B F. Highly constrained optimal launch ascent guidance. Journal of Guidance, Control, and Dynamics, 2010, 33(2): 404-414
