Volume 44 Issue 12
Dec.  2018
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CHEN Binghan, ZUO Zhengrong, XIA Luruiet al. Motion characteristic inversion method of single platform imaging target[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(12): 2528-2535. doi: 10.13700/j.bh.1001-5965.2018.0340(in Chinese)
Citation: CHEN Binghan, ZUO Zhengrong, XIA Luruiet al. Motion characteristic inversion method of single platform imaging target[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(12): 2528-2535. doi: 10.13700/j.bh.1001-5965.2018.0340(in Chinese)

Motion characteristic inversion method of single platform imaging target

doi: 10.13700/j.bh.1001-5965.2018.0340
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  • Corresponding author: ZUO Zhengrong, E-mail: zhrzuo@mail.hust.edu.cn
  • Received Date: 07 Jun 2018
  • Accepted Date: 13 Jul 2018
  • Publish Date: 20 Dec 2018
  • Aimed at inversion of target motion characteristics under single platform observation conditions, the model and method for reconstructing target spatial position and estimating motion parameters based on sequence images are proposed. To suppress the effect of atmospheric refraction on the accuracy of location reconstruction, it is proposed that the atmosphere is treated as a layered sphere, and the reverse tracking strategy is adopted to calculate the transmission path of light in each layer of the atmosphere in reverse, starting from the incident light of the imaging system. In summary, the target location is determined according to the intersection of the tracking path and the target launch plane. Furthermore, in order to reduce the effect of prior parameter errors such as launch plane, iterative estimation is adopted to search the optimal firing surface within the range of prior error, with the consistency of the target acceleration parameters as the optimization criterion, and the reconstruction error is corrected. Through the above process, the target trajectory and the motion parameters are obtained by inversion. Within the prior error range, the inversion location error is less than 200 m and the inversion velocity error is less than 60 m/s.

     

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