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IMM 알고리듬의 모드 계수 갱신 방법을 통한 레이돔 굴절률 추정

Radome Slope Estimation using Mode Parameter Renewal Method of IMM Algorithm

  • 투고 : 2017.09.07
  • 심사 : 2017.10.18
  • 발행 : 2017.10.31

초록

항공기 전면에 장착되는 레이돔은 표적을 탐색 및 추적하는 데에 있어서 기동 중에 발생하는 다양한 이유로 굴절오차를 야기할 수 있다. 이러한 굴절오차는 마이크로파 탐색기가 허상표적을 탐지하고 있는 것을 의미한다. 3차원 공간상에서 항공기에 장착된 레이돔의 굴절률을 추정하는 목적으로 일반적으로 알려진 상호작용 다중모델(Interactive Multiple Model, IMM) 알고리듬을 적용한다. 하지만, 레이돔 굴절률과 같은 불확실한 시스템 모델의 계수를 추정할 수 있음에도 예측값의 범위를 벗어날 때에는 추정 성능을 보장할 수 없다. 본 논문에서는 레이돔 굴절률의 예측값을 IMM 알고리듬의 모드 계수로 두고 예측값을 갱신하는 방법을 제안하며, 제안한 방법의 레이돔 굴절률 추정 성능을 확인한다.

A radome mounted on the front of an aircraft can cause refraction errors for various reasons that occur during maneuver in seeking and tracking a target. This refraction error means that the microwave seeker is detecting apparent target. An Interactive Multiple Model (IMM) algorithm is applied to estimate radome slope mounted on an aircraft in 3D space. However, even though the parameter of uncertain system model such as radome slope can be estimated, the estimated performance can not be guaranteed when it exceeds the range of the predicted value. In this paper, we propose a method to update the predicted value by using the radome slope as the mode parameter of the IMM algorithm, and confirm the radome slope estimation performance of the proposed method.

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참고문헌

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