Journal of the Korean Society for Aeronautical & Space Sciences (한국항공우주학회지)

The Korean Society for Aeronautical and Space Sciences (한국항공우주학회)
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Asynchronous Guidance Filter Design Based on Strapdown Seeker and INS Information

스트랩다운 탐색기 및 INS 정보를 이용한 비동기 유도필터 설계

  • Received : 2020.06.08
  • Accepted : 2020.10.13
  • Published : 2020.11.01
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Abstract

In this paper, we propose a guidance filter to estimate line of sight rate with strapdown seeker measurements and INS(Inertial Navigation System) information. The measurements of proposed guidance filter consisted of the LOS(Line of Sight) and relative position that can be calculated with the seeker's measurements, INS information and known target position, also the filter is based on an asynchronous filter to use outputs of the two sensors that are out of synchronous and period. Through the proposed filter, we can reduce the effect on parasitic loop that can be caused by using large time delay seeker and improve the estimation performance.

본 논문은 스트랩다운 탐색기 측정치와 INS 정보를 이용하여 시선각속도를 추정하는 유도필터 설계에 대해서 다룬다. 제안하는 유도필터는 탐색기 측정치와 유도탄 자세로부터 획득 가능한 시선각과 표적의 위치와 유도탄과의 상대 위치를 측정치로 하고 있으며, 주기 및 동기가 맞지 않는 두 센서의 출력을 사용하기 위해 비동기 필터를 기반으로 하고 있다. 제안한 방법을 통해 시간지연이 큰 탐색기 측정치를 사용함으로써 생길 수 있는 기생루프에 대한 영향을 줄이고 추정성능을 향상시킬 수 있다.

Keywords

References

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