红外制导弹药协同定位跟踪方法研究

臧路尧; 林德福; 杨哲; 王武刚

doi:10.3788/IRLA201847.0404008

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红外制导弹药协同定位跟踪方法研究

臧路尧, 林德福, 杨哲, 王武刚

文章导航 > 红外与激光工程 > 2018 > 47(4): 404008-0404008(7)

臧路尧, 林德福, 杨哲, 王武刚. 红外制导弹药协同定位跟踪方法研究[J]. 红外与激光工程, 2018, 47(4): 404008-0404008(7). doi: 10.3788/IRLA201847.0404008

引用本文:

臧路尧, 林德福, 杨哲, 王武刚. 红外制导弹药协同定位跟踪方法研究[J]. 红外与激光工程, 2018, 47(4): 404008-0404008(7). doi: 10.3788/IRLA201847.0404008

Zang Luyao, Lin Defu, Yang Zhe, Wang Wugang. Research on cooperative location and tracking approach of infrared guided munition[J]. Infrared and Laser Engineering, 2018, 47(4): 404008-0404008(7). doi: 10.3788/IRLA201847.0404008

Citation:

Zang Luyao, Lin Defu, Yang Zhe, Wang Wugang. Research on cooperative location and tracking approach of infrared guided munition[J]. Infrared and Laser Engineering, 2018, 47(4): 404008-0404008(7). doi: 10.3788/IRLA201847.0404008

红外制导弹药协同定位跟踪方法研究

doi: 10.3788/IRLA201847.0404008

1.
北京理工大学宇航学院,北京 100081;
2.
中国北方工业公司军贸技术研究院,北京 100053;
3.
西北工业集团有限公司,陕西西安 710043

基金项目:

北京理工大学基础研究基金（20130142017）

详细信息

作者简介:
臧路尧(1987-),男,博士生,主要从事飞行器制导与控制方面的研究。Email:luyao_jizi@126.com

中图分类号: TJ765.3

Research on cooperative location and tracking approach of infrared guided munition

1.
School of Aerospace,Beijing Institute of Technology,Beijing 100081,China;
2.
International Armament Research & Development Center,China North Industries Corp,Beijing 100053,China;
3.
Northwest Industries Group Co. Ltd,Xi'an 710043,China

摘要: 针对红外制导导弹无法直接测量弹目距离、视线角速度及目标加速度等制导信息，且单枚导弹的可观测量少，目标定位误差大的问题，考虑红外导引头的测量特性，利用多枚导弹与目标的几何关系对目标进行协同定位。建立多枚导弹对目标的协同跟踪模型，通过计算导弹间相对运动关系估算弹目距离，并将其作为伪量测量，结合导引头测角信息构建新的量测方程，利用卡尔曼滤波估计出弹目距离和视线角速度等制导信息。针对机动目标，研究了一种基于交互式多模型滤波方法，利用多个目标机动模型加权融合的方法来估计真实目标机动模型。数学仿真表明该方法有效提高了对固定/机动目标的估计精度。
- 协同定位 /
- 卡尔曼滤波 /
- 交互式多模型 /
- 目标机动
Abstract: Aiming at the problem that infrared guided missile cannot measure guidance information such as the relative distance, line of sight(LOS) rate and target acceleration directly, the observability of a single missile was less, and the target location error was large, considering the measurement characteristics of infrared seeker, geometrical relationship among multiple missiles and the target was used to locate the target cooperatively. Multiple missiles cooperative tracking the target model was established. The distance between missiles and the target was estimated by calculating the relative motion between missiles, and it was used as pseudo quantity measurement. The new measurement equation was constructed combined with the angle measurement information of seeker. The relative distance and LOS rate was estimated by Kalman filtering algorithm. Aiming at the maneuvering target, an interactive multiple model filtering cooperative tracking method was studied. The maneuvering model of real target was estimated by weighted fusion of multiple target maneuvering models. Simulation results show that the proposed method can effectively improve the estimation accuracy of the stationary/maneuvering target.
- cooperative location /
- Kalman filtering /
- interacting multiple model /
- maneuvering target

[1]	Sun Weimeng. Research on guidance law design with terminal impact angle constraints in air-to-surface guided weapon[D]. Changsha:National University of Defense Technology, 2008. (in Chinese)
[2]	Shi Yanlong. Application of nonlinear filtering in ballistic target tracking[D]. Nanjing:Nanjing University of Science and Technology, 2012. (in Chinese)
[3]	Chen T, Xu S. Approach guidance with double-line-of-sight measuring navigation constraint for autonomous rendezvous[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(3):678-687.
[4]	Wang Kai, Chen Tong, Xu Shijie. A method of double line-of-sight measurement relative navigation[J]. Acta Aeronauticaet Aeronautica Sinica, 2011, 32(6):1084-1091. (in Chinese)
[5]	Dong Jipeng, Tang Dong. An algorithm of target tracking based on two missiles cooperative location information[J]. Aero Weaponry, 2014(3):3-7. (in Chinese)
[6]	Wang Jiawei. Research on cooperative guidance and control for multiple interceptors[D]. Harbin:Harbin Institute of Technology, 2014. (in Chinese)
[7]	Ye Jikun, Lei Humin, Xue Dongfeng, et al. Multiple missiles cooperative tracking algorithm base on geometric relation[J]. System Engineering Theory and Practice, 2012, 32(10):2332-2338. (in Chinese)
[8]	Liu Yanfang. Research on end-game guidance law for interceptor missile based on differential game theory[D]. Harbin:Harbin Institute of Technology, 2014. (in Chinese)
[9]	Shaferman V, Oshman Y. Cooperative Interception in a Multi-Missile Engagement[C]//Guidance, Navigation, and Control and Co-located Conferences, 2009.
[10]	M W, B S, W W, et al. Cooperative Tracking of Moving Targets by a Team of Autonomous UAVs[C]//IEEE/AIAA Digital Avionics Systems Conference,2006:1-9.
[11]	Zarchan P. Representation of realistic evasive maneuvers by the use of shaping filters[J]. Journal of Guidance, Control, and Dynamics, 1979, 2(4):290-295.
[12]	Jeon I, Lee J, Tahk M. Homing guidance law for cooperative attack of multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(1):275-280.

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红外制导弹药协同定位跟踪方法研究

doi: 10.3788/IRLA201847.0404008

1. 北京理工大学宇航学院,北京 100081;

2. 中国北方工业公司军贸技术研究院,北京 100053;

3. 西北工业集团有限公司,陕西西安 710043

作者简介:
臧路尧(1987-),男,博士生,主要从事飞行器制导与控制方面的研究。Email:luyao_jizi@126.com

收稿日期: 2017-11-05
修回日期: 2017-12-03
刊出日期: 2018-04-25

基金项目:

北京理工大学基础研究基金（20130142017）

中图分类号: TJ765.3

关键词:

摘要: 针对红外制导导弹无法直接测量弹目距离、视线角速度及目标加速度等制导信息，且单枚导弹的可观测量少，目标定位误差大的问题，考虑红外导引头的测量特性，利用多枚导弹与目标的几何关系对目标进行协同定位。建立多枚导弹对目标的协同跟踪模型，通过计算导弹间相对运动关系估算弹目距离，并将其作为伪量测量，结合导引头测角信息构建新的量测方程，利用卡尔曼滤波估计出弹目距离和视线角速度等制导信息。针对机动目标，研究了一种基于交互式多模型滤波方法，利用多个目标机动模型加权融合的方法来估计真实目标机动模型。数学仿真表明该方法有效提高了对固定/机动目标的估计精度。

English Abstract

Research on cooperative location and tracking approach of infrared guided munition

1. School of Aerospace,Beijing Institute of Technology,Beijing 100081,China;

2. International Armament Research & Development Center,China North Industries Corp,Beijing 100053,China;

3. Northwest Industries Group Co. Ltd,Xi'an 710043,China

Received Date: 2017-11-05
Rev Recd Date: 2017-12-03
Publish Date: 2018-04-25

Keywords:

Abstract: Aiming at the problem that infrared guided missile cannot measure guidance information such as the relative distance, line of sight(LOS) rate and target acceleration directly, the observability of a single missile was less, and the target location error was large, considering the measurement characteristics of infrared seeker, geometrical relationship among multiple missiles and the target was used to locate the target cooperatively. Multiple missiles cooperative tracking the target model was established. The distance between missiles and the target was estimated by calculating the relative motion between missiles, and it was used as pseudo quantity measurement. The new measurement equation was constructed combined with the angle measurement information of seeker. The relative distance and LOS rate was estimated by Kalman filtering algorithm. Aiming at the maneuvering target, an interactive multiple model filtering cooperative tracking method was studied. The maneuvering model of real target was estimated by weighted fusion of multiple target maneuvering models. Simulation results show that the proposed method can effectively improve the estimation accuracy of the stationary/maneuvering target.

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红外制导弹药协同定位跟踪方法研究

doi: 10.3788/IRLA201847.0404008

作者简介: 臧路尧(1987-),男,博士生,主要从事飞行器制导与控制方面的研究。Email:luyao_jizi@126.com

Research on cooperative location and tracking approach of infrared guided munition

计量

出版历程

红外制导弹药协同定位跟踪方法研究

doi: 10.3788/IRLA201847.0404008

1. 北京理工大学 宇航学院,北京 100081; 2. 中国北方工业公司军贸技术研究院,北京 100053; 3. 西北工业集团有限公司,陕西 西安 710043

作者简介: 臧路尧(1987-),男,博士生,主要从事飞行器制导与控制方面的研究。Email:luyao_jizi@126.com

English Abstract

Research on cooperative location and tracking approach of infrared guided munition

1. School of Aerospace,Beijing Institute of Technology,Beijing 100081,China; 2. International Armament Research & Development Center,China North Industries Corp,Beijing 100053,China; 3. Northwest Industries Group Co. Ltd,Xi'an 710043,China

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作者简介:
臧路尧(1987-),男,博士生,主要从事飞行器制导与控制方面的研究。Email:luyao_jizi@126.com

1. 北京理工大学宇航学院,北京 100081;

2. 中国北方工业公司军贸技术研究院,北京 100053;

3. 西北工业集团有限公司,陕西西安 710043

作者简介:
臧路尧(1987-),男,博士生,主要从事飞行器制导与控制方面的研究。Email:luyao_jizi@126.com

1. School of Aerospace,Beijing Institute of Technology,Beijing 100081,China;

2. International Armament Research & Development Center,China North Industries Corp,Beijing 100053,China;

3. Northwest Industries Group Co. Ltd,Xi'an 710043,China