全捷联被动雷达末制导系统设计

doi:10.3969/j.issn.1001-506X.2020.11.24

Abstract

Abstract:

In order to solve the problem of precision guidance under the condition of large measurement error of the strapdown passive radar seeker, the terminal guidance system of strapdown passive radar is studied from the perspective of practical engineering application. Firstly, the strapdown passive radar seeker model is established. Secondly, in view of the problems of system nonlinearity, filter stability, calculation amount and the coupling of guidance and attitude control, a terminal guidance system scheme based on the algorithms of guidance information extraction with cubature Kalman filter (CKF), sliding mode variable structure guidance, three-loop overload pilot and so on is proposed. Finally, combined with the anti-radiation missile application scene, the system-wide simulation model is established for the scheme verification. The results show that the hit accuracy is 2 m when hitting the stationary target by using the designed terminal guidance system, and the system has a good adaptability for the slow moving target within 15 m/s, the impact point circular error probability (CEP) can reach about 10 m.

Key words: strapdown passive radar seeker, terminal guidance, cubature Kalman filter (CKF), sliding mode guidance law

CLC Number:

Chunming ZHAO, Yueming YAO, Wen JIN, Weiyang SONG, Haihong FANG. Design of terminal guidance system for strapdown passive radar[J]. Systems Engineering and Electronics, 2020, 42(11): 2607-2613.

Figures/Tables 14

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References 21

1	JAMES M M.Line of sight rate estimation for guided projectiles with strapdown seekers[C]//Proc.of the AIAA Guidance, Navigation and Control Conference, 2015: AIAA 2015-0344.
2	JACQUES W . Line-of-sight rate estimation and linearizing control of an imaging seeker in a tactical missile guided by proportional navigation[J]. IEEE Trans.on Control Systems Technology, 2002, 10 (4): 556- 567. doi: 10.1109/TCST.2002.1014675
3	WU H , CHEN S X , YANG B F , et al. Robust rang-parame-terized cubature Kalman filter for bearings-only tracking[J]. Journal of Central South University, 2016, 23 (6): 1399- 1405. doi: 10.1007/s11771-016-3192-z
4	WANG P, ZHANG K. Research on line-of-sight rate extraction of strapdown seeker[C]//Proc.of the 33rd Chinese Control Conference, 2014: 859-863.
5	SMITA S , CHOSHAL T K . Sight line rate estimaion in missile seeker using disturbance observer-based technique[J]. IEEE Trans.on Control Systems Technology, 2011, 19 (2): 449- 454. doi: 10.1109/TCST.2010.2046662
6	刘振亚, 高敏, 许路铁. 基于容积卡尔曼滤波的全捷联制导信息估计算法[J]. 探测与控制学报, 2017, 39 (6): 93- 98.
	LIU Z Y , GAO M , XUE L T . Strapdown guidance information estimation algorithm based on cubature Kalman filter[J]. Journal of Detection & Control, 2017, 39 (6): 93- 98.
7	王小刚, 胡智勇, 于洋, 等. 基于鲁棒滤波的捷联导引头视线角速度估计方法[J]. 中国惯性技术学报, 2016, 24 (2): 251- 256.
	WANG X G , HU Z Y , YU Y , et al. Line-of-sight angular-rate estimation of strapdown seeker based on robust filter[J]. Journal of Chinese Inertial Technology, 2016, 24 (2): 251- 256.
8	MI W H, SHAN J Y, LIU Y S. Adaptive unscented Kalman filter based line of sight rate for strapdown seeker[C]//Proc.of the Chinese Automation Congress, 2018: 886-891.
9	JANG S A, RYOO C K, CHOI K, et al. Guidance algorithms for tactical missiles with strapdown seeker[C]//Proc.of the SICE Annual Conference, 2008: 2616-2619.
10	庞威, 谢晓方, 刘家祺, 等. 改进粒子滤波的全捷联导引头制导信息估计[J]. 现代防御技术, 2018, 46 (1): 80- 87.
	PANG W , XIE X F , LIU J Q , et al. Guidance information estimation of full strap-down seeker with improved particle filter[J]. Modern Defence Technology, 2018, 46 (1): 4736- 4738.
11	张韬, 张希铭, 王民钢. 全捷联导引头制导信息滤波算法及仿真[J]. 西北工业大学学报, 2015, 33 (5): 744- 749.
	ZHANG T , ZHANG X M , WANG M G . Algorithm and simulation for guidance information filter for strap-down seekers[J]. Journal of Northwestern Polytechnical University, 2015, 33 (5): 744- 749.
12	袁亦方, 林德福, 祁载康. 单兵全捷联图像制导弹药制导信息估计技术[J]. 红外与激光工程, 2015, 44 (1): 370- 376.
	YUAN Y F , LIN D F , QI Z K . Techniques on estimating guidance information for strap-down image guided man portable munitions[J]. Infrared and Laser Engineering, 2015, 44 (1): 370- 376.
13	陈伟, 冯高鹏, 孙传杰, 等. 单兵火箭弹捷联导引滤波方法研究[J]. 飞行力学, 2017, 35 (3): 68- 72.
	CHEN W , FENG G P , SUN C J , et al. Research on filtering method for strapdown guidance of individual rocket projectile[J]. Flight Dynamics, 2017, 35 (3): 68- 72.
14	刘振亚, 高敏, 程呈. 基于理想弹道鲁棒容积卡尔曼滤波视线角估计[J]. 系统工程与电子技术, 2018, 40 (2): 409- 416.
	LIU Z Y , GAO M , CHENG C . Line-of-sight angle estimation algorithm based on ideal tralectory robust cubature Kalman filter[J]. Systems Engineering and Electronics, 2018, 40 (2): 409- 416.
15	KIM D, RYOO C K, KIM Y, et al. Guidance and control for missiles with a strapdown seeker[C]//Proc.of the 11th International Conference on Control, Automation and Systems, 2011: 969-972.
16	KATKURI J R, JILKOV V P, LI X R.A comparative study of nonlinear filters for target tracking in mixed coordinates[C]//Proc. of the 42nd South Eastern Symposium on System Theory, 2010: 202-207.
17	IENKARAN A , SIMON H . Cubature Kalman filters[J]. IEEE Trans.on Automatic Control, 2009, 54 (6): 1254- 1269. doi: 10.1109/TAC.2009.2019800
18	CHAO T, WANG S Y, YANG M.Angular constrained guidance law and its optimization with hybrid optimization algorithm[C]//Proc.of the IEEE Chinese Guidance, Navigation and Control Conference, 2014: 2455-2460.
19	LEE C H, KIM T H, TAHK M J, et al.Design of guidance law for passive homing missile using sliding mode control[C]//Proc.of the International Conference on Control, Automatic and Systems, 2010: 2380-2385.
20	YUN Y H, TANG S J, GUO J, et al.Adaptive sliding-mode guidance with terminal angle constraints based on explicit space engagement model[C]//Proc.of the IEEE Chinese Guidance, Navigation and Control Conference, 2016: 1144-1147.
21	ZHOU D , MU C D , XU W L . Adaptive sliding-mode guidance of a homing missile[J]. Journal of Guidance, Control, and Dynamics, 1999, 22 (4): 589- 594. doi: 10.2514/2.4421

仿真模式	目标静止	目标10 m/s	目标15 m/s
标称弹道	0.5	9.3	11.5
随机打靶	2.0	9.4	12.3

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[14]	HUANG Wei, XU Jian-cheng, WU Hua-xing. Trajectory control arithmetic of missile-borne SAR terminal guidance [J]. Systems Engineering and Electronics, 2016, 38(9): 2115-2121.
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Design of terminal guidance system for strapdown passive radar

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