Volume 44 Issue 1
Jan.  2018
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XIN Shijun, ZHENG Wei, WANG Yidiet al. Impact of pulsar angular position on pulse template and its compensation method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(1): 169-175. doi: 10.13700/j.bh.1001-5965.2016.0958(in Chinese)
Citation: XIN Shijun, ZHENG Wei, WANG Yidiet al. Impact of pulsar angular position on pulse template and its compensation method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(1): 169-175. doi: 10.13700/j.bh.1001-5965.2016.0958(in Chinese)

Impact of pulsar angular position on pulse template and its compensation method

doi: 10.13700/j.bh.1001-5965.2016.0958
Funds:

National Natural Science Foundation of China 10973048

More Information
  • Corresponding author: ZHENG Wei, E-mail: zhengwei@nudt.edu.cn
  • Received Date: 21 Dec 2016
  • Accepted Date: 20 Jan 2017
  • Publish Date: 20 Jan 2018
  • Recovering pulse template is one key technology of X-ray pulsar-based navigation system. Its precision is closely related to the pulsar angular position. First, this paper briefly introduced the theory of recovering standard profile. Then, the impact of pulsar angular position error on pulse template was analyzed and its analytical formula of annual mean value and the integral for any arc segment were derived. Finally, we proposed a feasible way that can significantly decrease the impact of pulsar angular position error. These research conclusions and simulation analysis verify the effectiveness of error compensation method, which could provide reference for optimizing observation task of X-ray pulsars and recovering X-ray pulse template.

     

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