变质心再入弹头螺旋机动突防弹道设计

doi:10.7527/S1000-6893.2016.0027

Abstract

Abstract:

To improve the penetrability of moving-mass reentry warhead, an actively spiral maneuver trajectory is proposed. Dynamics model and missile-target kinematics model are established and analyzed by introducinga new variable and controlling the lateral position of moving-mass; the angle between the velocity vector and the line of sight vector is controlled at a desired value. Based on the above analysis, analytical solutions of spiral maneuver radius and root-mean-square miss distance are derived. Six-dimensional trajectory simulations demonstrate that the proposed approach is capable of achieving spiral maneuver. By adjusting the value of maneuver margin, the spiral maneuver and high precision can be achieved at the same time.

Key words: spiral maneuver, hypersonic vehicle, moving-mass control, penetration, reentry

CLC Number:

V412

WANG Linlin, YU Jianqiao, WANG Yafei. Spiral maneuver penetration trajectory for moving-mass reentry warhead[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(5): 1484-1493.

References

[1] 高长生, 李君龙, 荆武兴, 等. 导弹质量矩控制技术发展综述[J]. 宇航学报, 2010, 31(2):307-314. GAO C S, LI J L, JING W X, et al. Key technique and development for moving mass actuated kinetic missile[J]. Journal of Astronautics, 2010,31(2):307-314(in Chinese).
[2] 李自行, 李高风. 移动质心再入飞行器建模及自抗扰滚动控制[J]. 航空学报, 2012, 33(11):2121-2129. LI Z X, LI G F. Moving centroid reentry vehicle modeling and active disturbance rejection roll control[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(11):2121-2129(in Chinese).
[3] MURPHY C H. Influence of moving internal parts on angular motion of spinning projectiles[J]. Journal of Guidance, Control, and Dynamics, 1978, 1(2):117-122.
[4] MURPHY C H. Symmetric missile dynamic instabilities[J]. Journal of Guidance, Control, and Dynamics, 1981, 4(5):464-471.
[5] ROGERS J, COSTELLO M. Flight dynamics and control authority of a projectile equipped with a controllable internal translating mass:AIAA-2007-6492[R]. Reston:AIAA,2007.
[6] ROGERS J, COSTELLO M. A variable stability projectile using an internal moving mass:AIAA-2008-7116[R]. Reston:AIAA, 2008.
[7] ROGERS J, COSTELLO M. Control authority of a projectile equipped with a controllable internal translating mass[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(5):1323-1333
[8] GRACEY C, CLIFF E M. Fixed-trim reentry guidance analysis[J]. Journal of Guidance, Control, and Dynamics, 1981, 5(6):558-563.
[9] GAO C S, JING W X, WEI P X. Research on application of single moving mass in the reentry warhead maneuver[J]. Aerospace Science and Technology, 2013, 30(1):108-118.
[10] MENON P K, SWERIDUK G D, OHLMEYER E J, et al. Integrated guidance and control of moving-mass actuated kinetic warheads[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(1):118-126.
[11] PETSOPOULOS T, REGAN F J, BARLOW J. Moving-mass roll control system for fixed-trim reentry vehicle[J]. Journal of Spacecraft and Rockets, 1996, 33(1):54-60.
[12] OHLMEYER E J. Root-mean-square miss distance of proportional navigation missile against sinusoidal target[J]. Journal of Guidance, Control, and Dynamics, 1996, 19(3):563-568.
[13] 崔静, 姜玉宪. 拦截导弹动力学特性对摆动式机动策略突防效果的影响[J]. 宇航学报, 2001, 22(5):33-38. CUI J, JIANG Y X. The effect of interceptor's dynamics system order on the penetration efficiency of weaving maneuver strategy[J]. Journal of Astronautics, 2001, 22(5):33-38(in Chinese).
[14] 顾文锦, 赵红超, 王凤莲, 等. 导弹末端机动的一体化控制模型[J]. 宇航学报, 2004, 25(6):677-680. GU W J, ZHAO H C, WANG F L, et al. Integrative control model of missiles' terminal maneuver[J]. Journal of Astronautics, 2004, 25(6):677-680(in Chinese).
[15] 顾文锦, 赵红超, 王凤莲. 反舰导弹末端机动的突防效果研究[J]. 宇航学报, 2005, 26(6):758-761. GU W J, ZHAO H C, WANG F L. Research on the penetration effect of terminal maneuver for anti-ship missiles[J]. Journal of Astronautics, 2005, 26(6):758-761(in Chinese).
[16] 郦苏丹, 任萱, 吴瑞林. 再入弹头的螺旋机动研究[J]. 宇航学报, 2000, 21(4):41-48. LI S D, REN X, WU R L. Research of spiral maneuver of reentrying missile[J]. Journal of Astronautics, 2000, 21(4):41-48(in Chinese).
[17] 秦建飞, 张义广, 李俊峰. 导弹末端机动与导引一体化设计的新机动模型[J]. 宇航学报, 2009, 30(5):1866-1870. QIN J F, ZHANG Y G, LI J F. A new maneuver model for integrated design of missiles' terminal maneuver and guidance[J]. Journal of Astronautics, 2009, 30(5):1866-1870(in Chinese).
[18] 张汝川, 顾文锦, 赵红超. 基于主动螺旋变轨的三维末制导律研究[J]. 兵工学报, 2009, 30(6):720-726. ZHANG R C, GU W J, ZHAO H C. Research on 3D terminal guidance laws based on actively self-homing spiral variable trajectory[J]. Acta Armamentarii, 2009, 30(6):720-726(in Chinese).
[19] 谢愈, 刘鲁华, 汤国建, 等. 高超声速滑翔飞行器摆动式机动突防弹道设计[J]. 航空学报, 2011, 32(12):2174-2181. XIE Y, LIU L H, TANG G J, et al. Weaving maneuver trajectory design for hypersonic glide vehicles[J]. Acta Aeronautica et Aeronautica Sinica, 2011, 32(12):2174-2181(in Chinese).
[20] 宋贵宝, 朱平云, 李红亮. 空舰导弹俯冲弹道螺旋机动制导律研究[J]. 兵工学报, 2014, 35(2):220-227. SONG G B, ZHU P Y, LI H L. Research on the guidance law for spiral maneuver of air-to-ship missile in dive trajectory phase[J]. Acta Armamentarii, 2014, 35(2):220-227(in Chinese).
[21] 王林林, 于剑桥, 王亚飞, 等. 单滑块变质心非对称再入飞行器建模及控制[J]. 系统工程与电子技术, 2015, 37(5):1116-1123. WANG L L, YU J Q, WANG Y F, et al. Single moving-mass asymmetrical reentry vehicle modeling and control[J]. Systems Engineering and Electronics, 2015, 37(5):1116-1123(in Chinese).
[22] 胡剑波, 陈新海. 多回路控制系统的标准系数设计法及其应用研究[J]. 系统工程与电子技术, 2004, 26(12):1852-1863. HU J B, CHEN X H. Standard coefficient design method for multi-loops control system and its application[J]. Systems Engineering and Electronics, 2004, 26(12):1852-1863(in Chinese).
[23] 王亚飞. 再入飞行器动力学特性与控制方法研究[D]. 北京:北京理工大学, 2015:97-98. WANG Y F. Research on dynamics and control methods of a reentry vehicle[D]. Beijing:Beijing Institute of Technology, 2015:97-98(in Chinese).

Spiral maneuver penetration trajectory for moving-mass reentry warhead

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Zhikun SUN, Zhiwei SHI, Weilin ZHANG, Zheng LI, Qijie SUN. Effect of plasma actuator on lift-drag characteristics of high-speed airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 23-39.
[2]	Zheng LI, Cong XU, Jian ZHANG, Mengmeng LI, Yilei MA, Guanghui BAI. Reverse jet flow control by plasma synthetic jet actuator in high speed flow field [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 225-232.
[3]	Zhengxue MA, Zhenbing LUO, Aihong ZHAO, Yan ZHOU, Wei XIE, Qiang LIU, Yinxin ZHU, Wenqiang PENG. Reverse jet characteristics of plasma synthetic jet in hypersonic flow field [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 192-203.
[4]	ZHENG Hui, QIU Lei, YUAN Shenfang, YANG Xiaofei, LU Xulong, XUE Zhaopeng. Experimental method of guided wave monitoring for high temperature airflow damage of C/C thermal protection structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 225659-225659.
[5]	SUN Cong. Development status, challenges and trends of strength technology for hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 527590-527590.
[6]	LUO Shibin, MIAO Zhichao, SONG Jiawen. Influencing factors of active cooling at leading edge of hypersonic vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 627023-627023.
[7]	ZHANG Daoyi, ZHOU Chaoying. Drag reduction and heat protection mechanism of annular jet and combined jet [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 126056-126056.
[8]	ZHOU Yinjia, ZHANG Zhixian, FU Xinwei, A Rong. Integrated computing method for ablative thermal protection system of reentry vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124520-124520.
[9]	GAO Chang, LI Zhengzhou, HUANG Jiangtao, HE Yuanyuan, WU Yingchuan, LE Jialing, GUI Feng. High-accuracy aerodynamic optimization of hypersonic vehicles based on continuous adjoint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124490-124490.
[10]	LIU Zhe, LU Haoran, ZHENG Wei, WEN Guoguang, WANG Yidi, ZHOU Xiang. Rapid time-coordination trajectory planning method for multi-glide vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524497-524497.
[11]	DING Yibo, YUE Xiaokui, DAI Honghua, CUI Naigang. Prescribed performance controller for flexible air-breathing hypersonic vehicle with considering inlet airflow constraint [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524838-524838.
[12]	LI Jiaxing, WANG Dayi, E Wei, GE Dongming. Autonomous navigation technology based on optical image under large dynamic disturbance [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(11): 524907-524907.
[13]	LI Shuaicong, HE Ruizhi, TANG Guojian, AO Peng. Profile tracking guidance law based on sliding mode control [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724578-724578.
[14]	WANG Yuqi, NING Guodong, WANG Xiaofeng, HAO Mingrui, WANG Jianghua. Maneuver penetration strategy of near space vehicle based on differential game [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S2): 724276-724276.
[15]	CHEN Bing, ZHENG Yong, CHEN Zhanglei, ZHANG Houtian, LIU Xinjiang. A review of celestial navigation system on near space hypersonic vehicle [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(8): 623686-623686.