Volume 47 Issue 4
Apr.  2018
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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

Research on cooperative location and tracking approach of infrared guided munition

doi: 10.3788/IRLA201847.0404008
  • Received Date: 2017-11-05
  • Rev Recd Date: 2017-12-03
  • Publish Date: 2018-04-25
  • 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.
  • [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.
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Research on cooperative location and tracking approach of infrared guided munition

doi: 10.3788/IRLA201847.0404008
  • 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

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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