基于大气数据传感器的协同制导控制方法

doi:10.3969/j.issn.1001-506X.2020.09.22

摘要/Abstract

摘要：

为研究多弹协同攻击的低成本实现问题,提出一种基于大气数据传感器的捷联导弹协同制导控制方法。首先,对协同制导控制中的状态反馈信息进行分析。然后,研究使用攻角传感器和皮托管代替陀螺仪提供制导控制所需的角度反馈信息的可行性,结合协同制导算法与自动驾驶仪设计方法研究基于大气数据传感器的协同制导控制方法。最后,对该方法进行初步的数值仿真验证。理论分析和仿真结果表明,基于大气数据传感器的捷联导弹协同制导控制具有理论可行性。

关键词: 大气数据传感器, 陀螺仪, 协同制导

Abstract:

In order to study the low-cost implementation problem of multi-missile cooperative attack, a cooperative guidance and control method of strapdown missile based on the air data sensor is proposed. Firstly, the state feedback information in cooperative guidance and control is analyzed. Then, the feasibility of using angle of attack sensors and pitot tubes instead of gyroscopes to provide the angle feedback information needed for guidance control is studied. The cooperative guidance algorithm and the design method of autopilot are also combined to study the cooperative guidance and control method based on the air data sensor. Finally, the method is preliminary verified by numerical simulation. The theoretical analysis and simulation results show that the cooperative guidance and control of strapdown missiles based on the air data sensor are theoretically feasible.

Key words: air data sensor, gyroscope, cooperative guidance

中图分类号:

TJ765

陈亚东, 陈中文, 王佳楠, 单家元. 基于大气数据传感器的协同制导控制方法[J]. 系统工程与电子技术, 2020, 42(9): 2060-2065.

Yadong CHEN, Zhongwen CHEN, Jianan WANG, Jiayuan SHAN. Cooperative guidance and control method based on air data sensor[J]. Systems Engineering and Electronics, 2020, 42(9): 2060-2065.

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参考文献 34

1	JEON I S , LEE J I , TAHK M J . Homing guidance law for cooperative attack of multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2010, 33 (1): 275- 280.
2	ZHANG Y A , WANG X L , WU H L , et al. A distributed cooperative guidance law for salvo attack of multiple anti-ship missiles[J]. Chinese Journal of Aeronautics, 2015, 28 (5): 1438- 1450. doi: 10.1016/j.cja.2015.08.009
3	ZHAO E J, CHAO T, WANG S Y, et al. Distributed cooperative guidance law for multiple flight vehicles of saturation attack[C]//Proc.of the AIAA Atmospheric Flight Mechanics Conference, 2016: 3240.
4	CHEN Y D , WANG J N , WANG C Y , et al. A modified cooperative proportional navigation guidance law[J]. Journal of the Franklin Institute, 2019, 356 (11): 5692- 5705. doi: 10.1016/j.jfranklin.2019.04.013
5	ZHOU J L , YANG J Y . Distributed guidance law design for coopera-tive simultaneous attacks with multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2016, 39 (10): 2436- 2445.
6	DHANANJAY N , GHOSE D . Accurate time-to-go estimation for proportional navigation guidance[J]. Journal of Guidance, Control, and Dynamics, 2014, 37 (4): 1378- 1383.
7	LI G F , WU Y J , XU P Y . Adaptive fault-tolerant cooperative guidance law for simultaneous arrival[J]. Aerospace Science and Technology, 2018, 82-83, 243- 251. doi: 10.1016/j.ast.2018.09.014
8	LI Z H , DING Z T . Robust cooperative guidance law for simultaneous arrival[J]. IEEE Trans.on Control Systems Technology, 2019, 27 (3): 1360- 1367.
9	ZHOU J L , YANG J Y . Guidance law design for impact time attack against moving targets[J]. IEEE Trans.on Aerospace & Electronic Systems, 2018, 54 (5): 2580- 2589.
10	HU Q L , HAN T , XIN M . Sliding-mode impact time guidance law design for various target motions[J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (1): 136- 148.
11	WANG J W , ZHANG R . Terminal guidance for a hypersonic vehicle with impact time control[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (8): 1790- 1798. doi: 10.2514/1.G003540
12	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): 132- 141.
13	WANG P Y , GUO Y N , MA G F , et al. New differential geome-tric guidance strategies for impact-time control problem[J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (9): 1982- 1992. doi: 10.2514/1.G004229
14	TEKIN R , ERER K S , HOLZAPFEL F . Adaptive impact time control via look-angle shaping under varying velocity[J]. Journal of Guidance, Control, and Dynamics, 2017, 40 (12): 3247- 3255. doi: 10.2514/1.G002981
15	CHEN X T , WANG J Z . Nonsingular sliding-mode control for field-of-view constrained impact time guidance[J]. Journal of Guidance, Control, and Dynamics, 2018, 41 (5): 1214- 1222.
16	HAN T , HU Q L , XIN M . Analytical solution of field-of-view limited guidance with constrained impact and capturability analysis[J]. Aerospace Science and Technology, 2020, 97, 105586. doi: 10.1016/j.ast.2019.105586
17	AI X L , WANG L L , YU J Q , et al. Field-of-view constrained two-stage guidance law design for three-dimensional salvo attack of multiple missiles via an optimal control approach[J]. Aerospace Science and Technology, 2019, 85, 334- 346. doi: 10.1016/j.ast.2018.11.052
18	CHEN Y D , WANG J N , XIN M , et al. Three-dimensional coope-rative homing guidance law with field-of-view constraint[J]. Journal of Guidance, Control, and Dynamics, 2019, 43 (2): 389- 397.
19	HE S M , HE W , LIN D F , et al. Consensus-based two-stage salvo attack guidance[J]. IEEE Trans.on Aerospace & Electronic Systems, 2018, 54 (3): 1555- 1566.
20	ZHOU J L , YANG J Y , LI Z K . Simultaneous attack of a stationary target using multiple missiles: a consensus-based approach[J]. Science China Information Sciences, 2017, 60 (7): 070205. doi: 10.1007/s11432-016-9089-7
21	KANG S , WANG J N , LI G , et al. Optimal cooperative guidance law for salvo attack: an MPC-based consensus perspective[J]. IEEE Trans.on Aerospace & Electronic Systems, 2018, 54 (5): 2397- 2410.
22	ZHANG Y , TANG S J , GUO J . Two-stage cooperative guidance strategy using a prescribed-time optimal consensus method[J]. Aerospace Science and Technology, 2020, 100, 105641. doi: 10.1016/j.ast.2019.105641
23	ZHAO Q L , DONG X W , LIANG Z X , et al. Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies[J]. Chinese Journal of Aeronautics, 2017, 30 (4): 1570- 1581. doi: 10.1016/j.cja.2017.06.009
24	HOU D L , WANG Q , SUN X J , et al. Finite-time cooperative guidance laws for multiple missiles with acceleration saturation constraints[J]. IET Control Theory & Applications, 2015, 9 (10): 1525- 1535.
25	贺敏, 王晓芳, 林海. 信息单向传输带拦截角约束的协同拦截制导律[J]. 系统工程与电子技术, 2019, 41 (8): 1827- 1834.
	HE M , WANG X F , LIN H . Cooperative intercept guidance law with intercept angle constraint based on one-way information transmission[J]. Systems Engineering and Electronics, 2019, 41 (8): 1827- 1834.
26	CHEN X T , WANG J Z . Sliding-mode guidance for simulta-neous control of impact time and angle[J]. Journal of Guidance, Control, and Dynamics, 2019, 42 (2): 394- 401.
27	KANG S , TEKIN R , HOLZAPFEL F . Generalized impact time and angle control via look-angle shaping[J]. Journal of Guidance, Control, and Dynamics, 2018, 42 (3): 695- 702.
28	ZHANG Y A , MA G X , LIU A L . Guidance law with impact time and impact angle constraints[J]. Chinese Journal of Aeronautics, 2013, 26 (4): 960- 966. doi: 10.1016/j.cja.2013.04.037
29	ZHU J W , SU D L , XIE Y . Impact time and angle control guidance independent of time-to-go prediction[J]. Aerospace Science and Technology, 2019, 86, 818- 825. doi: 10.1016/j.ast.2019.01.047
30	HARL N , BALAKRISHNAN S N . Impact time and angle guidance with sliding mode control[J]. IEEE Trans.on Control Systems Technology, 2012, 20 (6): 1436- 1449. doi: 10.1109/TCST.2011.2169795
31	HOU Z W , YANG Y , LIU L . Terminal sliding mode control based impact time and angle constrained guidance[J]. Aerospace Science and Technology, 2019, 93, 105142. doi: 10.1016/j.ast.2019.04.050
32	李桂英, 于志刚, 张扬. 带有角度约束的机动目标拦截协同制导律[J]. 系统工程与电子技术, 2019, 41 (3): 626- 635.
	LI G Y , YU Z G , ZHANG Y . Cooperative guidance law with angle constraint to intercept maneuvering target[J]. Systems Engineering and Electronics, 2019, 41 (3): 626- 635.
33	钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2012.
	QIAN X F , LIN R X , ZHAO Y N . Missile flight mechanics[M]. Beijing: Press of Beijing Institute of Technology, 2012.
34	林德福, 王辉, 王江, 等. 战术导弹自动驾驶仪设计与制导律分析[M]. 北京: 北京理工大学出版社, 2012.
	LIN D F , WANG H , WANG J , et al. Autopilot design and guidance law analysis for tactical missiles[M]. Beijing: Press of Beijing Institute of Technology, 2012.

系数	T_m	ζ_m	A₁	A₂	$ k_{\dot{\vartheta}}$	k_α	k_a	T_α	B₁	—
取值	0.081 4	0.135 9	0.004 0	0.001 5	0.302 7	0.348 4	90.799 6	1.155 1	-0.001 3	—

导弹	弹目距离/m	视线角/(°)	弹道倾角/(°)
1	10 000	-30	-15
2	12 000	-35	5

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[11]	肖冰松, 方洋旺, 胡诗国, 曾宪伟. 多机空战协同制导决策方法[J]. Journal of Systems Engineering and Electronics, 2009, 31(3): 610-612.
[12]	李清东, 陈璐璐, 张孝功, 任章. FADS快速智能故障检测和诊断技术[J]. Journal of Systems Engineering and Electronics, 2009, 31(10): 2544-2546.