Volume 44 Issue 4
Apr.  2018
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Article Contents
WANG Ershen, YANG Fuxia, PANG Tao, et al. BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 684-690. doi: 10.13700/j.bh.1001-5965.2017.0277(in Chinese)
Citation: WANG Ershen, YANG Fuxia, PANG Tao, et al. BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(4): 684-690. doi: 10.13700/j.bh.1001-5965.2017.0277(in Chinese)

BDS/GPS combined navigation receiver autonomous integrity monitoring algorithm

doi: 10.13700/j.bh.1001-5965.2017.0277
Funds:

National Natural Science Foundation of China 61571309

National Natural Science Foundation of China 61101161

the Fundamental Research Funds for the Central Universities 3132016317

Liaoning BaiQianWan Talents Program 

Program for Liaoning Excellent Talents in University LR2016069

Scientific Study Project for Liaoning Province Ministry of Education L201716

Aeronautical Science Foundation of China 2015ZC54010

More Information
  • Corresponding author: WANG Ershen, E-mail: wes2016@126.com
  • Received Date: 03 May 2017
  • Accepted Date: 19 May 2017
  • Publish Date: 20 Apr 2018
  • In order to make receiver autonomous integrity monitoring (RAIM) technique be applied to approach with vertical guidance (APV) flight phase in civil aviation navigation, the BDS/GPS combined navigation RAIM algorithm is studied. An algorithm based on the optimal weighted average solution of BDS/GPS position solution is proposed. Combined with the relationship between the optimal weighted average solution and BDS/GPS position solution, a test statistic is established. The test threshold is obtained according to the maximum allowable false alarm probability, and then the satellite navigation system fault is detected. Through the weighted least squares residual method, the satellite fault is detected and identified. The results are instructive for the study of multi-constellation combined satellite navigation system applied to the navigation in civil aviation APV flight phase.

     

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