基于反预警的反拦截中段规避突防策略

doi:10.7527/S1000-6893.2016.0116

Abstract

Abstract:

An anti-warning-based anti-interception avoiding penetration strategy is proposed for fully exploiting potential of the multi-pulse maneuvering and improving the midcourse penetration ability of ballistic missiles. With the interception system being regarded as threats and transformed into the constraint conditions, the multi-pulse trajectory design is turned into an obstacle avoidance path planning for the unmanned aerial vehicle, wherein the pulse ignition point and interval are regarded as the search nodes and step, respectively. The optimal ignition parameters are selected based on a comprehensive consideration of the detection system delay and the performance and deployment of the interception system. Influence of pulse increment and system delay on multi-pulse trajectory is studied Simulation results show that the proposed strategy can damage the convergence of enemy's prediction algorithm by multi-pulse maneuvering, and the accuracy of hostile warning results is thus reduced. When the enemy's prediction error sufficiently converges and the hostile warning is accurate enough, the missile is already being out of the range of interception. According to the latest information in battlefield, an optimal multi-pulse trajectory can be designed offline in 60 s, which can increase (decrease) the flight altitude and the average flight speed, and shorten (prolong) the flight time by 20%-35%.

Key words: ballistic missile, multi-pulse, threat, obstacle avoidance, ballistic design, maneuvering penetration

CLC Number:

V448.131

ZHOU Qihang, LIU Yanfang, QI Naiming, YAN Junfeng. Anti-warning-based anti-interception avoiding penetration strategy in midcourse[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(1): 319922-319922.

References

[1] 鲜勇, 李少朋, 雷刚, 等. 弹道导弹中段机动突防技术研究综述[J]. 飞航导弹, 2015, 18(9):43-46. XIAN Y, LI S P, LEI G, et al. Discussion of ballistic missile penetrating missile defense system[J]. Aerodynamic Missile Journal, 2015, 18(9):43-46(in Chinese).
[2] 周啟航, 张刘, 霍明英, 等. 弹道导弹中段突防弹道设计与验证[J]. 光学精密工程, 2015, 36(9):2645-2655. ZHOU Q H, ZHANG L, HUO M Y. et al. Ballistic missile midcourse penetration trajectory design and validation[J]. Optics and Precision Engineering, 2015, 36(9):2645-2655(in Chinese).
[3] 鲜勇, 李少朋, 李振华, 等. 基于梯度粒子群算法的纵横向机动跳跃弹道设计及优化[J]. 弹道学报, 2015, 27(3):1-6. XIAN Y, LI S P, LI Z H, et al. Design and optimization of vertical wavy and crosswise maneuvering trajectory based on grads particle swarm algorithm[J]. Journal of Ballistics, 2015, 27(3):1-6(in Chinese).
[4] 李广华, 张洪波, 汤国建. 高超声速滑翔飞行器典型弹道特性分析[J]. 宇航学报, 2015, 46(4):397-403. LI G H, ZHANG H B, TANG G J. Typical trajectory characteristics of hypersonic glide vehicle[J]. Journal of Astronautics, 2015, 46(4):397-403(in Chinese).
[5] 鲜勇, 刘炳琪, 王安民, 等. 变射面弹道横向转弯飞行程序的设计与优化[J]. 弹道学报, 2014, 26(4):30-35. XIAN Y, LIU B Q, WANG A M, et al. Design and optimization of lateral turning flight programon changeable launching plane trajectory[J]. Journal of Ballistics, 2014, 26(4):30-35(in Chinese).
[6] 明超, 孙瑞胜, 白宏阳, 等. 基于hp自适应伪谱法的多脉冲导弹弹道优化设计[J]. 固体火箭技术, 2015, 38(2):151-155. MING C, SUN R S, BAI H Y, et al. Optimizing design of trajectory for multiple-pulse missiles based on hp-adaptive pseudo-spectral method[J]. Journal of Solid Rocket Technology, 2015, 38(2):151-155(in Chinese).
[7] 邓逸凡, 李超兵, 王志刚. 一种基于轨道要素形式终端约束的航天器空间变轨迭代制导算法[J]. 航空学报, 2015, 36(6):1975-1982. DENG Y F, LI C B, WANG Z G. An iterative guidance algorithm using orbit element as terminal constraints for spacecraft orbit transfer[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(6):1975-1982(in Chinese).
[8] 冯令兵, 葛致磊, 李宪强, 等. 弹道导弹被动段最优脉冲变轨方法[J]. 指挥控制与仿真, 2014, 36(2):114-117. FENG L B, GE Z L, LI X Q, et al. A study on the ballistic missile's optimal impulse orbit transfer in the passive ballistic curve[J]. Command Control Simulation, 2014, 36(2):114-117(in Chinese).
[9] GILLIS M P I. Optimal mid-course modication of ballistic missile trajectories:Air Force Institute of Technology Report[R]. Washington, D.C.:Wright-Patterson Air Force Base, 1975.
[10] DRUCKMANN E, BENASHER J Z. Optimal in-flight trajectory modifications for ballistic missiles and free rockets[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(2):462-470.
[11] GUO Y, YAO Y, WANG S, et al. Maneuver control strategies to maximize prediction errors in ballistic middle phase[J]. Journal of Guidance, Control, and Dynamics, 2013, 36(4):1225-1234.
[12] GUO Y, YAO Y, WANG S, et al. Maneuver strategy of evader considering detection system[C]//Proceedings of AIAA Guidance, Navigation, and Control Conference. Reston:AIAA, 2011.
[13] 张广明, 高普云, 唐乾刚. 导弹在被动段突防的脉冲式异面变轨方法[J]. 宇航学报, 2008, 29(1):89-94. ZHANG G M, GAO P Y, TANG Q G. The method of the impulse trajectory transfer in a different plane for the ballistic missile penetrating missile defense system in the passive ballistic curve[J]. Journal of Astronautics, 2008, 29(1):89-94(in Chinese).
[14] 高普云, 张广明, 唐乾刚, 等. 导弹在被动段突防的脉冲式轴向加速方法[J]. 宇航学报, 2008, 29(4):1126-1130. GAO P Y, ZHANG G M, TANG Q G, et al. The method of increasing velocity along its original velocity direction by the impulse firing for the ballistic missile to penetrate the anti-missile system in the passive ballistic curve[J]. Journal of Astronautics, 2008, 29(4):1126-1130(in Chinese).
[15] 高普云, 张广明, 冯志刚, 等. 基于脉冲点火弹头空间机动的被动段弹道设计方法和数值仿真[J]. 宇航学报, 2009, 30(3):884-889. GAO P Y, ZHANG G M, FENG Z G, et al. The method of the trajectory design and numerical stimulation of the missile maneuvers in space based on the impulse firing in the passive curve[J]. Journal of Astronautics, 2009, 30(3):884-889(in Chinese).
[16] 张斌, 任军学, 王一白, 等. 导弹在被动段轴向加速变轨弹道设计与优化[J]. 北京航空航天大学学报, 2010, 21(6):650-653. ZHANG B, REN J X, WANG Y B. Design and optimization on trajectory of increasing velocity along its original velocity direction by impulse firing for ballistic missile to penetrate anti-missile system in passive ballistic curve[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 21(6):650-653(in Chinese).
[17] 赵秀娜. 机动弹头的智能规避策略研究[D]. 长沙:国防科学技术大学, 2006:10-25. ZHAO X N. The intelligent evasive strategy of the maneuver missiles[D]. Changsha:National University of Defense Technology, 2006:10-25(in Chinese).
[18] 丁明跃, 郑昌文, 周成平, 等. 无人飞行器航迹规划[M]. 北京:电子工业出版社, 2009:49-50. DING M Y, ZHENG C W, ZHOU C P, et al. Flight path planning for unmanned aerial vehicles[M]. Beijing:Electronics Industry Press, 2009:49-50(in Chinese).
[19] 张广明, 高普云, 唐乾刚, 等. 弹道导弹在被动段突防的平面脉冲式变轨方法[J]. 弹道学报, 2008, 34(3):83-86. ZHANG G M, GAO P Y, TANG Q G, et al. The method of the impulse trajectory transfer in a plane for the ballistic missile breaking through a defense line in the passive ballistic curve[J]. Journal of Ballistics, 2008, 34(3):83-86(in Chinese).
[20] 贾沛然, 陈克俊, 何力. 远程火箭弹道学[M]. 长沙:国防科技大学出版社, 1993:173-199. JIA P R, CHEN K J, HE L. Long-range rocket ballistics[M]. Changsha:National University of Defense Technology Press, 1993:173-199(in Chinese).
[21] 刘暾, 赵钧. 空间飞行器动力学[M]. 哈尔滨:哈尔滨工业大学出版社, 2003:62-68. LIU D, ZHAO J. Aero spacecraft dynamics[M]. Harbin:Harbin Institute of Technology Press, 2003:62-68(in Chinese).
[22] 赵钧. 航天器轨道动力学[M]. 哈尔滨:哈尔滨工业大学出版社, 2011:42-87. ZHAO J. Orbital dynamics ofspacecraft[M]. Harbin:Harbin Institute of Technology Press, 2011:42-87(in Chinese).odication of Ballistic Missile Trajectories, ” Air Force Inst. of Technology Report[S]. AD-A019333, Wright-Patterson Air Force Base, OH, 1975.
[10]Druckmann E, Ben-Asher J Z.Optimal In-Flight Tra-jectory Modifications for Ballistic Missiles and Free Rockets[J].Journal of Guidance, Control, and Dynam-ics, 2012, 35(2):462-470
[11]Guo Y, Yao Y, Wang S, et al.Maneuver Control Strate-gies to Maximize Prediction Errors in Ballistic Middle Phase[J].Journal of Guidance, Control, and Dynamics, 2013, 36(4):1225-1234
[12]Guo Y, Yao Y, Wang S, et al.Maneuver Strategy of Evader Considering Detection System[C].AIAA Guidance, Navigation, and Control Conference 08 - 11 Au-gust 2011, Portland, Oregon
[13]张广明, 高普云, 唐乾刚.导弹在被动段突防的脉冲式异面变轨方法[J].宇航学报, 2008, 29(1):89-94
[14]高普云, 张广明, 唐乾刚, 等.导弹在被动段突防的脉冲式轴向加速方法[J].宇航学报, 2008, 29(4):1126-1130
[15]高普云, 张广明, 冯志刚, 等.基于脉冲点火弹头空间机动的被动段弹道设计方法和数值仿真[J].宇航学报, 2009, 30(3):884-889
[16]张斌, 任军学, 王一白, 等. 弹道导弹在被动段轴向加速变轨弹道设计与优化[J]. 北京航空航天大学学报, 2010,21(6): 650-653.
[17]赵秀娜.机动弹头的智能规避策略研究[D].国防科学技术大学, 2006.
[18]丁明跃，郑昌文，周成平，等无人飞行器航迹规划[M].电子工业出版社, 2009.49-50.
[19]贾沛然, 陈克俊, 何力.远程火箭弹道学[M]. 国防科技大学出版社, 1993.173-199
[20]刘暾，赵钧.空间飞行器动力学[M].哈尔滨：哈尔滨工业大学出版社，2003: 62-68
[21]赵钧.航天器轨道动力学[M].哈尔滨：哈尔滨工业大学出版社，2011: 42-87

Anti-warning-based anti-interception avoiding penetration strategy in midcourse

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	HE Yuting. On the generalized survivability of aircraft and its evaluation method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526118-526118.
[2]	PANG Lei, CAO Zhiqiang, YU Junzhi. A pedestrian-aware collision-free following approach for mobile robots based on A^* and TEB [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524909-524909.
[3]	GE Jiahao, LIU Li, DONG Xinxin, TIAN Weiyong, LU Tianhe. Trajectory planning for free floating space robots based on kinodynamic RRT^* [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(1): 523877-523877.
[4]	TIAN Bailing, LI Pinpin, LU Hanchen, ZONG Qun. Trajectory and attitude coordinated control of multiple unmanned aerial vehicles (UAVs) in complex environments [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724245-724245.
[5]	XI Zhifei, XU An, KOU Yingxin, LI Zhanwu, YANG Aiwu. Target threat assessment in air combat based on PCA-MPSO-ELM algorithm [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(9): 323895-323895.
[6]	ZHAO Yanqin, CHEN Renliang. Systematical modelling of low-altitude windshear and its qualitative threat analysis to helicopter flight safety [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 123413-123413.
[7]	WANG Siyuan, WANG Gang, YUE Shaohua, SONG Yafei, LIU Jiayi. Threat assessment based on multilayer and multistage skyline selection method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(5): 323494-323494.
[8]	CHEN Qi, ZHAO Min, LI Yuhui, HE Ziyang. Optimal segment constant trajectory planning for parafoil system based on gradient descent method [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 324226-324226.
[9]	ZHANG Yunpu, SHAN Ganlin. Multi-sensor management approach for aerial target threat assessment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(11): 323218-323218.
[10]	LIU Jianghui, LI Haiyang, LU Lin, ZHAO Jian. Hybrid potential function safety guidance for approaching uncontrolled rotating target spacecraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(10): 323068-323068.
[11]	HUANG Tisheng, ZHAO Min, JIANG Li, WANG Pengfei, CAO Xiwei. Design method for interior ballistics of solid launch vehicle motor [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(S1): 722186-722186.
[12]	MA Guangfu, DONG Hongyang, HU Qinglei. Fault-tolerant translational control for spacecraft formation flying with collision avoidance requirement [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(10): 321129-321129.
[13]	YU Dateng, WANG Hua, SUN Fuyu. Optimal evasive maneuver strategy with potential threatening area being considered [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(1): 320202-320202.
[14]	FU Xiaowei, LI Jinliang, GAO Xiaoguang. Defense Penetration Path Planning for UCAV Based on Threat Netting [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(4): 1042-1052.
[15]	YU Jianguo, LIU Mei, CHEN Jinhai. Ballistic Target Track Segments Association and Optimization [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(10): 1897-1904.