[1] 周伟, 李毅, 张亚迪. 外军巡航导弹发展态势分析[J]. 航天电子对抗, 2015, 31(1): 1-5. Zhou W, Li Y, Zhang Y D. nalysis of the Development Situation of Foreign Military Cruise Missiles[J]. Aerospace Electronic Competition, 2015, 31(1): 1-5. [2] 杨希祥, 杨慧欣, 王鹏. 伪谱法及其在飞行器轨迹优化设计领域的应用综述[J]. 国防科技大学学报, 2015(4):1-8. Yang X X, Yang H X, Wang P.Overview of pseudo-spectral method and its application in trajectory optimum design for flight vehicles[J]. Journal of National University of Defense Technology, 2015(4):1-8. [3] Ross I M, Fahroo F.A Unified Computational Framework for Real-Time Optimal Control[C]// Proceedings of the 42nd IEEE Conierence on Decision and Control. Maui, Hawaii USA: IEEE Press, 2003: 2210-2215. [4] Ross I M, Sekhavat P, Fleming A, et al.Optimal Feedback Control: Foundations, Examples,and Experimental Results for a New Approach[J]. Journal of Guidance,Control and Dynamics (S0731-5090), 2008, 31(2): 1307-1321. [5] Tian B, Zong Q.Optimal guidance for reentry vehicles based on indirect Legendre pseudospectral method[J]. Acta Astronautica (S0094-5765), 2011, 68(7/8): 1176-1184. [6] 黄诘, 张友安, 刘永新, 等. 基于Radau伪谱方法的轨迹优化[J]. 海军航空工程学院学报, 2015, 30(4): 315-320. Huang J, Zhang Y A, Liu Y X, et al.Trajectory optimization based on Radau pseudospectral method[J]. Journal of Naval Aeronautical Engineering Institute, 2015, 30(4): 315-320. [7] 明超, 孙瑞胜, 白宏阳, 等. 基于hp自适应伪谱法的多脉冲导弹弹道优化设计[J]. 固体火箭技术, 2015(2):151-155. Ming C, Sun R S, Bai H Y, et al.Ballistic optimization design of multi-pulse missile based on hp adaptive pseudospectral method[J]. Solid State Rocket Technology, 2015(2): 151-155. [8] Peng H, Gao Q, Wu Z, et al.Optimal guidance based on receding horizon control for low-thrust transfer to libration point orbits[J]. Advances in Space Research, 2013, 51(11): 2093-2111. [9] Darby C L, Hager W W, Rao A V.Direct trajectory optimization using a variable low-order adaptive pseudospectral method[J]. Journal of Spacecraft and Rockets (S0022-4650). 2011, 48(3): 433-445. [10] Lu P.Closed-form control laws for linear time-varying systems[J]. Automatic Control (S0018-9286), IEEE Transactions on, 2000, 45(3): 537-542. [11] 吴森堂. 飞航导弹制导控制系统随机鲁棒分析与设计[M]. 北京: 国防工业出版社, 2010: 39-200. WU Sentang.Tochastic robustness analysis and design for guid-ance and control systemof winged missile[M]. Beijing: NationalDefense Industry Press, 2010: 39-200. [12] 韩祖南. 国外著名导弹解析[M]. 北京: 国防工业出版社, 2013: 198-203. Han Z N.Analysis of famous foreign missiles[M]. Beijing: National Defence Industry Press, 2013: 198-203. |