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Implementation of ZUPT on RPA Navigation System for GNSS Denied Ground Test

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주제분류기타공학

초록

In this paper, Zero velocity UPdaTe (ZUPT) is implemented on the navigation system of Remotely Piloted Aircraft for GNSS denied environment. RPA’s navigation system suffers from lack or loss of satellite signal while maintenance or ground test inside a hangar. Although some of the hangars install GPS repeaters for indoor tests, the anti-jamming equipment with array antenna blocks the repeater signal regarding them as hostile jamming signal. With ZUPT, an aircraft navigation system can be tested free from the divergence of navigation solution without line-of-sight satellites. The designed ZUPT aided centralized Kalman Filter is implemented on the Embedded GPS&INS and simulated with Captive Flight Test data. The simulation result shows stable navigation solution without GNSS updates.

Abstract

In this paper, Zero velocity UPdaTe (ZUPT) is implemented on the navigation system of Remotely Piloted Aircraft for GNSS denied environment. RPA’s navigation system suffers from lack or loss of satellite signal while maintenance or ground test inside a hangar. Although some of the hangars install GPS repeaters for indoor tests, the anti-jamming equipment with array antenna blocks the repeater signal regarding them as hostile jamming signal. With ZUPT, an aircraft navigation system can be tested free from the divergence of navigation solution without line-of-sight satellites. The designed ZUPT aided centralized Kalman Filter is implemented on the Embedded GPS&INS and simulated with Captive Flight Test data. The simulation result shows stable navigation solution without GNSS updates.

참고문헌 (8)

  1. Manuel Appel, "Experimental validation of GNSS repeater detection based on antenna arrays for maritime applications", CEAS Space Journal, 11(1), pp.7~19 (2019), Springer Science and Business Media LLC[DOI]
  2. 조성윤, "Stable Zero-Velocity Detection Method Regardless of Walking Speed for Foot-Mounted PDR", Journal of Positioning, Navigation, and Timing, 9(1), pp.33~42 (2020), 사단법인 항법시스템학회[DOI]
  3. "IEEE Aerospace and Electronic Systems Magazine", 2015, 42~69, pp.Institute of Electrical and Electronics Engineers (IEEE), https:
  4. An Urgent Need To Address Harmful Interferences to GNSS, "International Civil Aviation Organization", ICAO Technical Commission, ~ (2019)
  5. 이태규, "방위각 개선을 위한 SDINS", GPS, 한국군사과학기술학회지, pp.2006, 9(1)[DOI]
  6. Salychev, O. S, "Applied Inertial Navigation: Problems and Solutions" (2004), BMSTU Press
  7. 신현철, "무인항공기용 관성", 위성, 제어.로봇.시스템학회 논문지, pp.2018, 24(8)[DOI]
  8. 신현철, "High-degree Cubature Kalman Filtering Approach for GPS Aided In-Flight Alignment of SDINS", Journal of Positioning, Navigation, and Timing, 4(4), pp.181~186 (2015), 사단법인 항법시스템학회[DOI]

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