[1] [1] Raghav Harini Venkatesan, Nandan Kumar Sinha. Key factors that affect the performance of flares against a heat-seeking air-to-air missile[J]. The Journal of Defense Modeling and Simulation: Applications, Methodology, Technology, 2014, 11(4): 387-401.

[2] [2] Giovanni Franzini, Luca Tardioli, Lorenzo Pollini, et al. Visibility augmented proportional navigation guidance[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(4): 983-991.

[3] [3] XU Yang, FANG Yangwang, WU Youli, et al. Proportional guidance intelligent regulation strategy under the infrared interference and maneuvering[J]. Journal of National University of Defense Technology, 2019, 41(3): 137-145.

[4] [4] Paul Zarchan. Tactical and strategic missile guidance[M]. the 6th, AIAA, 2012.

[5] [5] WANG Xiaohai, MENG Xiuyun, ZHOU Feng, et al. Sliding mode guidance law with impact angle constraint based on bias proportional navigation[J]. Systems Engineering and Electronics, 2021, 43(5): 1295-1302.

[6] [6] LI Kebo, LIANG Yangang, SU Wenshan, et al. Performance of 3D TPN against true-arbitrarily maneuvering target for exoatmospheric interception[J]. Science China Technological Sciences, 2018, 61(8): 1161-1174.

[7] [7] LEE Suwon, LEE Youngjun, LEE Seokwon, et al. Data-driven capturability analysis for pure proportional navigation guidance considering target maneuver[J]. International Journal of Aeronautical and Space Sciences, 2021,22(5): 1209-1221.

[8] [8] LI Kebo, LIAO Xuanping, LIANG Yangang, et al. Guidance strategy with impact angle constraint based on pure proportional navigation[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(S2): 724277.

[9] [9] Satadal Ghosh, Debasish Ghose, Soumyendu Raha. Composite guidance for impact angle control against higher speed targets[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(1): 98-117.

[10] [10] LI Kebo, LIANG Yangang, SU Wenshan, et al. Performance of 3D TPN against true-arbitrarily maneuvering target for exoatmospheric interception[J]. Science China Technological Sciences, 2018, 61(8): 1161-1174.

[11] [11] FENG Tyan. The capture region of a general 3D TPN guidance law for missile and target with limited maneuverability[C]//Proc. American Control Conference, 2001: 512-517.

[12] [12] BAI Zhihui, LI Kebo, SU Wenshan, et al. Capture region of RTPN guidance law against arbitrarily maneuvering targets[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(8): 323947.

[13] [13] SHI Zhenqing, LIANG Xiaolong, ZHANG Jiaqiang, et al. Modeling and simulation analysis of 3-D air-to-air missile attack zone under the condition of target maneuvers[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2019, 39(3): 97-106.

[14] [14] Ernst-Christian Koch. Review on pyrotechnic aerial infrared decoys[J]. Propellants, Explosives, Pyrotechnics, 2011, 26(1): 3-11.

[15] [15] Ilan Rusnak. Bounds on the root-mean-square miss of radar-guided missiles against sinusoidal target maneuvers[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(4): 1066-1069.

[16] [16] Fumiaki Imado and Sachio Uehara. High-g barrel roll maneuvers against proportional navigation from optimal control viewpoint[J]. Journal of Guidance, Control, and Dynamics, 1988, 21(6): 876-881.

[17] [17] Timo Sailaranta, Ari Siltavuori, Antti Pankkonen. Simple missile models against high-g barrel roll maneuver[C]//Proc. AIAA Guidance, Navigation, and Control Conference, 2011: 01-12.

[18] [18] Ernst Christian Koch, Arno Hahma, Volker Weiser, et al. Metal-Fluorocarbon Pyrolants. XIII: High performance infrared decoy flare compositions based on MgB2 and Mg2Si and polytetrafluoroe-thylene/viton[J]. Propellants Explosives Pyrotechnics, 2010, 35: 1-7.

[19] [19] Srinivasan Ramaswam, David A Vaitekunas, Willem H Gunter, et al. Improvements to the ShipIR/NTCS adaptive track gate algorithm and 3D flare particle model[C]//Proc. SPIE Defense + Security, 2017, 10178: 1-12.

[20] [20] LI Shaoyi, ZHANG Kai, YIN Jianfei, et al. Study on IR target recognition approach in aerial jamming environment based on bayesian probabilistic model[J]. IEEE Access, 2019, 7: 50300-50316.

[21] [21] SHI Chen. Research on target recognition for anti-jamming towards infrared decoys[D]. Chengdu: University of Electronic Science and Technology of China, 2020.

[22] [22] Martin Weiss. Adjoint method for missile performance analysis on state space models[J]. Journal of Guidance, Control and Dynamics, 2005, 28(2): 236-248.

[23] [23] Martin Weiss, Domenic Bucco. Adjoint method for hybrid guidance loop state-space models[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(4): 614-622.

[24] [24] Martin Weiss, Domenic Bucco. Evaluation method for dual phase guided weapons based on the adjoint method[C]//Proc. AIAA Guidance, Navigation and Control Conference and Exhibit, 2007: 1-12.

[25] [25] LI Quancheng, FAN Yonghua, WAN Shizheng, et al. Influence of the seeker blind range guidance policy on guidance precision[C]//Proc. IEEE 9th Annual International Conference on CYBER Technology in Automation, Control, and Intelligent Systems (CYBER), 2019: 1120-1124.

[26] [26] Vitaly Shalumov, Tal Shima. Weapon–target-allocation strategies in multiagent target–missile–defender engagement[J]. Journal of Guidance, Control and Dynamics, 2017, 40(10): 2452-2464.

[27] [27] Domenic Bucco and Martin Weiss. Blind range influence on guidance loop performance: an adjoint-based analysis[C]//Proc. AIAA Guidance, Navigation, and Control Conference, 2013: 1-16.

[28] [28] WANG Weiqiang, JIA Xiaohong, FU Kuisheng, et al. Guidance precision analysis based on airborne IRCM stochastic process[J]. Infrared Technology, 2019, 41(2): 163-170.

[29] [29] Arthur Vermeulen, Gerrit Maes. Missile avoidance maneuvres with simultaneous decoy deployment[C]//Proc. AIAA Guidance, Navigation, and Control Conference, 2009: 1-17.

[30] [30] HUANG Hesong, TONG Zhongxiang, LI Taorui, et al. Defense strategy of aircraft confronted with IR guided missile[J]. Mathematical Problems in Engineering, 2017, 2017: 1-9.

[31] [31] Hecht C. Homing guidance using angular acceleration of the line of sight[C]//Proc. Navigation & Control Conference, 1991: 856-869.

[32] [32] Satadal Ghosh, Debasish Ghose, Soumyendu Raha. Unified time-to-go algorithms for proportional navigation class of guidance[J]. Journal of Guidance, Control and Dynamics, 2016, 39(6): 1188-1205.