[1] 索统一, 郑志强. 直升机载空地导弹关键技术研究[J]. 兵工学报, 2010, 31(2): 157-162. SUO T Y, ZHENG Z Q. Research on key techniques of helicopter-borne air to ground missiles[J]. Acta Armamentarii, 2010, 31(2): 157-162. (in Chinese)
[2] 邹汝平. 多用途导弹系统设计[M]. 北京: 国防工业出版社, 2018: 462-464. ZOU R P. Design of multi-purpose missile system[M]. Beijing: National Defense Industry Press, 2018: 462-464. (in Chinese)
[3] 陈建江. 面向飞航导弹的多学科稳健优化设计方法及应用[D]. 武汉: 华中科技大学, 2004. CHEN J J. Method and application of winged missile oriented multidisciplinary robust design optimization [D]. Wuhan: Huazhong University of Science & Technology, 2004. (in Chinese) [4] 马应, 何麟书, 邓家褆. 应用6σ质量控制方法的空射巡航导弹概念设计[J]. 固体火箭技术, 2010, 33(6): 616-620. MA Y, HE L S, DENG J T. The application of 6σ quality control approach to conceptual design of air launched cruise missiles[J]. Journal of Solid Rocket Technology, 2010, 33(6): 616-620. (in Chinese) [5] JAEGER L, GOGU C, SEGONDS S, et al. Aircraft multidisciplinary design optimization under both model and design variables uncertainty[J]. Journal of Aircraft , 2013, 50(2): 528-538. [6] 刘常青. 基于概率偏差的战术导弹总体方案设计技术[D]. 长沙: 国防科学技术大学, 2011. LIU C Q. System design technique of tactical missiles based on probabilistic deviations[D]. Changsha: National University of Defense Technology, 2011.(in Chinese)
[7] PISARONI M, NOBILE F, LEYLAND P. Continuation multilevel Monte Carlo evolutionary algorithm for robust aerodynamic shape design[J]. Journal of Aircraft, 2019, 56(2): 771-786. [8] VAN NGUYEN N, CHOI S M, KIM W S, et al. A multidisciplinary robust optimization framework for UAV conceptual design [J]. Aerospace Science and Technology, 2013, 26: 200-210. [9] 赵民, 刘百奇, 粟华. 面向飞行器总体设计的UMDO技术综述[J]. 宇航学报, 2018, 39(6): 593-604. ZHAO M, LIU B Q, SU H. Review of UMDO for system design of flight vehicle[J]. Journal of Astronautics, 2018, 39(6): 593-604. (in Chinese)
[10] 王刚, 胡峪, 宋笔锋. 考虑重心位置不确定性的无尾无人机优化设计[J]. 航空学报, 2015, 36(7): 2214-2224. WANG G, HU Y, SONG B F. Tailless UAV design and optimization under center of gravity location uncertainty[J]. Acta Aeronautics et Astronautica Sinica, 2015, 36(7): 2214-2224. (in Chinese) [11] RICARDO M P, CURRAN C, AFZAL S. Robust reliability-based design optimization framework for wing design[J]. AIAA Journal , 2014, 52(4): 711-724. [12] 王钦龙, 王红岩, 芮强. 基于多目标遗传算法的高速履带车辆动力学模型参数修正研究[J]. 兵工学报, 2016, 37(6): 969-978. WANG Q L, WANG H Y, RUI Q. Research on parameter updating of high mobility tracked vehicle dynamic model based on multi-objective genetic algorithm[J]. Acta Armamentarii, 2016, 37(6): 969-978. (in Chinese) [13] MELIN T. A vortex lattice MATLAB implementation for linear aerodynamic wing applications[D]. Stockholm,Sweden: Royal Institute of Technology, 2000. [14] 王刚. 一种利用螺旋桨动力配平的小型电动无尾无人机研究[D]. 西安: 西北工业大学, 2016. WANG G. A research on a small electric-powered tailless UAV using propeller thrust trimming[D]. Xi'an: Northwestern Polytechnical University, 2016.
[15] 《飞机设计手册》总编委会. 飞行设计手册:气动设计[M]. 北京: 航空工业出版社, 2002: 269-270. Aircraft Design Manual General Editorial Board. Aircraft design manual: aerodynamic design[M]. Beijing: Aviation Industry Press, 2002: 269-270. (in Chinese)
[16] 王刚, 刘钧圣, 王琨, 等. 一种亚声速导弹气动力计算方法研究[J]. 弹箭与制导学报, 2018, 38(2): 65-68. WANG G, LIU J S, WANG K, et al. A method to predict aerodynamic characteristics for subsonic missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2018, 38(2): 65-68.(in Chinese) [17] FLEEMAN E L. Tactical missile design[M]. Reston, US: American Institute of Aeronautics and Astronautics Inc., 2001. [18] 谷良贤, 温炳恒. 导弹总体设计原理[M]. 西安: 西北工业大学出版社, 2004: 115, 121. GU L X, WEN B H. Missile conceptual design[M]. Xi'an: Northwestern Polytechnical University Press, 2004: 115, 121. (in Chinese)
[19] 杨慧, 宋文萍, 韩忠华, 等. 旋翼翼型多目标多约束气动优化设计[J]. 航空学报, 2012, 33(7): 1218-1226. YANG H, SONG W P, HAN Z H, et al. Multi-objective and multi-constrained optimization design for a helicopter rotor airfoil[J]. Acta Aeronautics et Astronautica Sinica, 2012, 33(7): 1218-1226. (in Chinese) [20] 韩忠华. Kriging模型及代理优化算法研究进展[J]. 航空学报, 2016, 37(11): 3197-3225. HAN Z H. Kriging surrogate model and its application to design optimization[J]. Acta Aeronautics et Astronautica Sinica, 2016, 37(11): 3197-3225. (in Chinese)
第41卷第2期 2020 年2月兵工学报ACTA ARMAMENTARIIVol.41No.2Feb.2020
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