Citation: | Yu Lei, Fu Zhaowang, Li Zhanwu, et al. Guidance and control optimization method for fighter with threat avoidance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 229-234. (in Chinese) |
[1] |
强胜, 龙汉, 申镇, 等.追踪法推广的数学建模与仿真[J].兵工学报, 2009, 30(1):56-62 Qiang Sheng, Long Han, Shen Zhen, et al.Generalized mathematical model and simulations of pursuit guidance method[J].Acta ArmamentarⅡ, 2009, 30(1):56-62(in Chinese)
|
[2] |
赵文成, 那岚, 金学英.准平行接近法导引律的研究与实现[J].测控技术, 2009, 28(3):92-95 Zhao Wencheng, Na Lan, Jin Xueying.Research and realization of quasi-parallel approaching method[J].Observation and Control Technology, 2009, 28(3):92-95(in Chinese)
|
[3] |
王辉, 林德福, 祁载康.时变最优的增强型比例导引及其脱靶量解析解[J].红外与激光工程, 2013, 42(3):692-698 Wang Hui, Lin Defu, Qi Zaikang.Time-varying optimal augmented proportional navigation and miss distance closed-formed solution[J].Infrared and Laser Engineering.2013, 42(3):692-698(in Chinese)
|
[4] |
Tyan F, Shen J F.A simple adaptive GIPN missile guidance law[C]//Proceedings of the 2006 American Control Conference.Minneapolis, Minnesota, USA:IEEE, 2006:345-350
|
[5] |
周荻.寻的导弹新型导引规律[M].北京:国防工业出版社, 2002 Zhou Di.New guidance law for homing missile[M].Beijing:National Defense Press, 2002(in Chinese)
|
[6] |
冯艳清, 周红丽, 程凤舟, 等.带末端攻击角度约束的三维最优导引律研究[J].战术导弹技术, 2011(5):81-85 Feng Yanqing, Zhou Hongli, Cheng Fengzhou, et al.Study of three-dimensional optimal guidance law with terminal constraints[J].Tactical Missile Technology, 2011(5):81-85(in Chinese)
|
[7] |
Rusnak I.Optimal guidance laws with uncertain time-of-flight against maneuvering target and noisy measurements[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit.Austin, Texas:AIAA, 2003:5576-1-5576-8
|
[8] |
Ryoo C K, Cho H, Tahk M J.Time-to-go weighted optimal guidance with impact angle constraints[J].IEEE Transactions on Control Systems Technology, 2006, 14(3):483-492
|
[9] |
Wang Zhigang, Li Wei.Three dimensional optimal guidance law for micro missiles to attack maneuvering targets[J].Informatics in Control, Automation and Robotics, 2012, 133(5):283-286
|
[10] |
Menon P K A, Duke E L.Time-optimal aircraft pursuit evasion with a weapon envelope constraint[J].Journal of Guidance Control and Dynamics, 1992, 15(2):448-456
|
[11] |
Zhan Z H, Zhang J, Li Y.An efficient ant colony system based on receding horizon control for the aircraft arrival sequencing and scheduling problem[J].IEEE Transactions on Intelligent Transportation Systems, 2010, 11(2):399-412
|
[12] |
唐国金, 罗亚中, 雍恩米.航天器轨迹优化理论、方法及应用[M].北京:科学出版社, 2012 Tang Guojin, Luo Yazhong, Yong Enmi.Theory, method and application of trajectory optimization for spacecraft[M].Beijing:Science Press, 2012(in Chinese)
|
[13] |
Huntington G T, Benson D, Anil V R.A comparison of accuracy and computational efficiency of three pseudospectral method[J].AIAA Guidance, Navigation and Control Conference and Exhibit South Carolina, 2007:6405-6429
|
[14] |
Dua V, Bozinis N A, Pistikopoulos E N.A multi-parametric programming approach for mixed-integer quadratic engineering problems[J].Computer and Chemical Engineering, 2002, 26(4): 715-733
|
[15] |
Horie K, Conway B A.Optimal fighter pursuit-evasion maneuvers found via two-sided optimization[J].Journal of Guidance, Control, and Dynamics, 2006, 29(1):105-112
|
[16] |
Gill P E, Murray W, Saunders M A.SNOPT:an SQP algorithm for large-scale constrained optimization[J].SIAM Journal on Optimization, 2002, 12(4):979-1006
|