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Volume 44 Issue 9
Sep.  2022
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LU Dan, ZHAO Weizhen, ZHONG Lunlong. Airborne Global Navigation Satellite System Spoofing Interference Autonomous Detection Algorithm Based on Inertial Navigation System/Distance Measuring Equipment-Aided[J]. Journal of Electronics & Information Technology, 2022, 44(9): 3195-3202. doi: 10.11999/JEIT210640
Citation: LU Dan, ZHAO Weizhen, ZHONG Lunlong. Airborne Global Navigation Satellite System Spoofing Interference Autonomous Detection Algorithm Based on Inertial Navigation System/Distance Measuring Equipment-Aided[J]. Journal of Electronics & Information Technology, 2022, 44(9): 3195-3202. doi: 10.11999/JEIT210640

Airborne Global Navigation Satellite System Spoofing Interference Autonomous Detection Algorithm Based on Inertial Navigation System/Distance Measuring Equipment-Aided

doi: 10.11999/JEIT210640
Funds:  The Fundamental Research Funds for the Central Universities (3122019050), The Natural Science Foundation of Tianjin (19JCQNJC01000)
  • Received Date: 2021-06-28
  • Accepted Date: 2022-01-12
  • Rev Recd Date: 2022-01-09
  • Available Online: 2022-02-02
  • Publish Date: 2022-09-19
  • Global Navigation Satellite System (GNSS) spoofing causes the target receiver to generate incorrect positioning results. Using Inertial Navigation System (INS)-aided, constructing chi-squared test statistics based on the Kalman filter innovation sequence is an effective means to detect airborne GNSS spoofing. However, the algorithm cannot give the spoofing duration, causing the INS/GNSS system could not to determine whether the calculated positioning information is correct based on the algorithm. In this paper, a limited-memory chi-squared detection based on the reconstructed innovation sequence is proposed by using the Distance Measuring Equipment (DME) system. The algorithm uses the existing INS, GNSS and DME data to construct an innovation sequence that does not participate in Kalman filter, and then constructs the innovation sequence into a limited memory chi-square test statistic to detect spoofing interference. When the airborne GNSS spoofing causes a position deviation of 250 m and above, the designed algorithm can obtain a more accurate spoofing duration in simulation part. Finally, this paper gives the correct positioning information of the INS/GNSS/DME system based on the detection result of the proposed algorithm.
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