一种综合优势下的空空导弹接力制导混合优化方法
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摘要
基于综合制导优势函数提出了一种接力制导的遗传粒子群混合优化方法。通过建立飞机对导弹的优势模型、飞机对目标的态势优势模型、敌方飞机对我方飞机的威胁度模型以及作战飞机效能优势模型四个子模型,给出了作战飞机综合制导优势评估模型。结合接力制导约束条件,建立以综合制导优势最大为目标的空空导弹中制导权移交决策模型,并给出了基于遗传粒子群混合算法的空空导弹接力制导优化方法。最后,对八架飞机接力制导四枚空空导弹的情况进行仿真,验证了该模型及算法的有效性和正确性。
A genetic particle swarm hybrid method for relay guidance is proposed based on the integrated guidance superiority functions. Firstly, an integrated model for evaluating the guidance superiority of the combat aircraft is established by establishing four sub-models: the superiority model of aircraft to missile, the situational superiority model of aircraft to target, the threat model of enemy aircraft to our aircraft, and the efficiency superiority model of combat aircraft. In addition, considering the constraints of relay guidance, we establish a decision-making model for handing over the guidance power of an air-to-air missile with the goal of maximizing the integrated guidance superiority, and the optimization method of the air-to-air missile relay guidance based on the genetic particle swarm hybrid algorithm is given. Finally, we simulate the process of eight aircraft relaying guidance for four air-to-air missiles, and the simulation results verify the validity and correctness of the model and algorithm.
A genetic particle swarm hybrid method for relay guidance is proposed based on the integrated guidance superiority functions. Firstly, an integrated model for evaluating the guidance superiority of the combat aircraft is established by establishing four sub-models: the superiority model of aircraft to missile, the situational superiority model of aircraft to target, the threat model of enemy aircraft to our aircraft, and the efficiency superiority model of combat aircraft. In addition, considering the constraints of relay guidance, we establish a decision-making model for handing over the guidance power of an air-to-air missile with the goal of maximizing the integrated guidance superiority, and the optimization method of the air-to-air missile relay guidance based on the genetic particle swarm hybrid algorithm is given. Finally, we simulate the process of eight aircraft relaying guidance for four air-to-air missiles, and the simulation results verify the validity and correctness of the model and algorithm.
引文
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[13] 吕腾,吕跃勇,李传江,等. 带视线角约束的多导弹有限时间协同制导率[J]. 兵工学报, 2018, 39(2):305-314. [Lyu Teng, Lv Yue-yong, Li Chuan-jiang, et al. Finite time cooperative guidance law for multiple missiles with line of sight angle constraint[J]. Acta Armamentarii, 2018, 39(2):305-314.]
[14] Wang L, Yao Y, He FH. A novel cooperative mid-course guidance scheme for multiple intercepting missiles[J]. Chinese Journal of Aeronautics, 2017, 30(3):1140-1153.
[15] Zhao Q L,Dong X W,Liang Z X. Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies[J]. Chinese Journal of Aeronautics, 2017, 30(4):1570-1581.
[16] 冉华明,周锐,吴江,等. 超视距空战中多机协同制导方法[J]. 北京航空航天大学学报, 2014, 10:1547-1642. [Ran Hua-ming, Zhou Rui, Wu Jiang, et al. Cooperative guidance of multi aircraft in beyond-visual-range air combat[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 10:1547-1642.]
[17] Garcia E, Casbeer D W, Fuchs Z E. Cooperative missile guidance for active defense of air vehicles[J]. IEEE Tran-saction on Aerospace & Electronic Systems,2017,(99):1-1.
[18] Zhao J B, Yang S X. Integrated cooperative guidance framework and cooperative guidance law for multi-missile[J]. Chinese Journal of Aeronautics,2018,31(3):546-555.
[19] 费爱国,张陆游,刘刚,等.基于粒子群拍卖吻合算法的空空导弹制导权移交技术[J].宇航学报,2013,34(3):213-219.[Fei Ai-guo,Zhang Lu-you,Liu gang, et al. The technology for air-to-air missile gui-dance superiority handover based on particle swarm auction hyb-rid algorithm[J]. Journal of Astronautics, 2013, 34(3): 213-219.]
[2] 黄清禄,王在华,姬刚丽,等.“网络中心战”作战效能评价[J].四川兵工学报,2012,33(7):69-71. [Huang Qing-lu, Wang Zai-hua, Ji Gang-li. “Network Center Warfare” combat effectiveness evaluation[J]. Journal of Sichuan Ordnance,2012,33(7):69-71.]
[3] 王君,芮同林,李进,等. 空空导弹网络化协同制导作战模式[J]. 航空兵器, 2015(5):32-35. [Wang Jun, Rui Tong-lin, Li Jin, et al. The networking cooperative guidance combat pattern for air-to-air missile[J]. Aero Weaponry, 2015(5):32-35.]
[4] Gao Y, Zhou J, Guo J. Multi-missile distributed cooperative guidance law based on network synchronization principle[J]. Control Conference, 2016, 23(14):8150-8153.
[5] Diao X H, Fang Y W. Cooperative midcourse guidance handover law for mid-long-range air-to-air missile[J]. Electronics Optics & Control,2015,11(3):5-14.
[6] 周德云,杨振,张堃. 多UCAV超视距协同空战中的交接制导方法[J]. 弹道学报, 2017, 29(2):1-7. [Zhou De-yun, Yang Zhen, Zhang Kun. Method of guidance handover in beyond-visual-range coordinated air-combat for multi-UCAVs[J]. Journal of Ballistics, 2017, 29(2):1-7.]
[7] 何应圳. 编队协同接力制导仿真研究[J]. 现代计算机, 2016, 3(13):1007-1010. [He Ying-zhen. Research on the simulation of relay guidance of formation coordination[J]. Modern Computer, 2016, 3(13):1007-1010.]
[8] Shin H S. Study on cooperative missile guidance for area air defence[D].Cranfield:Cranfield University,2010.
[9] Kumar S R, Shima T. Cooperative nonlinear guidance strategies for aircraft defense[J]. Journal of Guidance Control & Dynamics, 2016, 40(1): 1-15.
[10] Piet-Lahanier H, Kahn A, Marzat J. Cooperative guidance laws for maneuvering target interceptions[J]. Automatic Control in Areospace, 2013.
[11] Lee W, Bang H. Analysis of A new cooperative guidance law for improved target tracking by multiple UAVs[C]. International Conference on Control, Automation and Systems, Korea, 2011.
[12] 宋俊红,宋申民,徐胜利. 一种拦截机动目标的多导弹协同制导率[J]. 宇航学报,2016,37(12):1306-1314. [Song Jun-hong, Song Shen-min, Xu Sheng-li. A cooperative guidance law for multiple missiles to intercept maneuvering target[J]. Journal of Astronautics, 2016,37(12):1306-1314.]
[13] 吕腾,吕跃勇,李传江,等. 带视线角约束的多导弹有限时间协同制导率[J]. 兵工学报, 2018, 39(2):305-314. [Lyu Teng, Lv Yue-yong, Li Chuan-jiang, et al. Finite time cooperative guidance law for multiple missiles with line of sight angle constraint[J]. Acta Armamentarii, 2018, 39(2):305-314.]
[14] Wang L, Yao Y, He FH. A novel cooperative mid-course guidance scheme for multiple intercepting missiles[J]. Chinese Journal of Aeronautics, 2017, 30(3):1140-1153.
[15] Zhao Q L,Dong X W,Liang Z X. Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies[J]. Chinese Journal of Aeronautics, 2017, 30(4):1570-1581.
[16] 冉华明,周锐,吴江,等. 超视距空战中多机协同制导方法[J]. 北京航空航天大学学报, 2014, 10:1547-1642. [Ran Hua-ming, Zhou Rui, Wu Jiang, et al. Cooperative guidance of multi aircraft in beyond-visual-range air combat[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 10:1547-1642.]
[17] Garcia E, Casbeer D W, Fuchs Z E. Cooperative missile guidance for active defense of air vehicles[J]. IEEE Tran-saction on Aerospace & Electronic Systems,2017,(99):1-1.
[18] Zhao J B, Yang S X. Integrated cooperative guidance framework and cooperative guidance law for multi-missile[J]. Chinese Journal of Aeronautics,2018,31(3):546-555.
[19] 费爱国,张陆游,刘刚,等.基于粒子群拍卖吻合算法的空空导弹制导权移交技术[J].宇航学报,2013,34(3):213-219.[Fei Ai-guo,Zhang Lu-you,Liu gang, et al. The technology for air-to-air missile gui-dance superiority handover based on particle swarm auction hyb-rid algorithm[J]. Journal of Astronautics, 2013, 34(3): 213-219.]