[1] 杨希祥, 降振宇, 张为华. 基于粒子群优化的固体运载火箭上升段弹道优化设计研究[J]. 宇航学报, 2010, 31(5): 1304-1309. YANG Xi-xiang, JIANG Zhen-yu, ZHANG Wei-hua. Solid rocket based on particle swarm optimization on the ballistic optimization design research [J]. Journal of Aerospace, 2010, 31(5):1304-1309.(in Chinese) [2] 傅阳光, 周成平, 丁明跃. 基于混合量子粒子群优化算法的三维航迹规划[J]. 宇航学报, 2010, 31(12): 2657-2664. FU Yang-guang, ZHOU Cheng-ping, DING Ming-yue. Quantum particle swarm optimization algorithm based on hybrid 3D path planning [J]. Journal of Aerospace, 2010, 31(12):2657-2664. (in Chinese) [3] Kennedy J, Eberhart R. Particle swarm optimization[C]∥IEEE International Joint Conference on Neural Networks. Perth, Austra-lia: IEEE, 1995:1942-1948. [4] Afshar M H. Large scale reservoir operation by constrained particle swarm optimization algorithms [J]. Journal of Hydro-environment Research, 2012, 6(1):75-87.
[5] Michalewicz Z, Dasgupta D, Riche R, et al. Evolutionary algorithms for constrained engineering problems[J]. Computers & Industrial Engineering, 1996, 30(4):851-870. [6] Bouallègue S, Haggège J, Benrejeb M. Particle swarm optimization-based fixed-structure H∞ control design[J]. International Journal of Control, Automation, and Systems,2011, 9(2):258-266. [7] Cai H L. A new adaptive penalty function in the application of genetic algorithm[J]. Journal of East China Normal University:Natural Science, 2015, 6(6):36-52. [8] Sedlaczek K, Eberhard P. Using augmented Lagrangian particle swarm optimization for constrained problems in engineering[J]. Structural and Multidisciplinary Optimization, 2006, 32(4):277-286. [9] Kim T H, Maruta I, Sugie T. Robust PID controller tuning based on the constrained particle swarm optimization[J]. Automatica, 2008, 44(4):1104-1110.
[10] Liang J J, Runarsson T P, Mezura-Montes E, et al. Problem de-finitions and evaluation criteria for the CEC 2006 special session on constrained real-parameter optimization[EB/OL]. [2006-09-18]. http:∥www.lania.mx/~emezura/util/files/tr_cec06.pdf. [11] 郑 建华, 杨涤. 鲁棒控制理论在倾斜转弯导弹中的应用[M]. 北京:国防工业出版社, 2001. ZHENG Jian-hua, YANG Di. Robust control theory in the application of bank missile[M]. Beijing: National Defense Industry Press, 2001. (in Chinese) [12] Doyle J C. A review of μ for case studies in robust control[C]∥10th IFAC Triennial World Congress. Munich, FRG:Pergamon Press, 1988:365-370. [13] Li T J, Ma Y J. Robust vibration control flexble tensegrity structure via μ synthesis[J]. Structure Control and Health Monitoring, 2013, 20(2):173-186. [14] 李伟杰,沈作军. 基于μ分析的高超声速飞行器再入轨迹评估[J]. 飞行力学, 2016, 34(4):50-53, 58. LI Wei-jie, SHEN Zuo-jun. An evaluation of hypersonic vehicle reentry trajectory based on μ-analysis[J]. Flight Dynamics, 2016, 34(4):50-53, 58.(in Chinese) [15] Doyle J C, John C, Chu C C. Matrix interpolation and H∞ performance bounds[C]∥American Control Conference. Boston, MA:IEEE,1985:129-134. [16] 臧月进. 空-空导弹μ综合控制器设计与研究[D]. 南京:南京航空航天大学, 2012. ZANG Yue-jin. The design and research of μ-Air-to-air Missile integrated controller[J]. Nanjing:Nanijng University of Aeronautics and Astronautics, 2012.(in Chinese)
第38卷 第1期2017 年1月兵工学报ACTA ARMAMENTARIIVol.38No.1Jan.2017
|