Sensor Redundancy Management using Kalman Filter for a Duplex Filght Control System

칼만필터를 이용한 2중 비행제어시스템의 센서 다중화 관리

  • 이승현 (한국항공우주연구원 항공연구본부 비행제어팀) ;
  • 이장호 (한국항공우주연구원 항공연구본부 비행제어팀) ;
  • 김응태 (한국항공우주연구원 항공연구본부 비행제어팀) ;
  • 성기정 (한국항공우주연구원 항공연구본부 비행제어팀)
  • Received : 2010.11.10
  • Accepted : 2010.12.20
  • Published : 2010.12.31

Abstract

This paper presents a duplex flight control system of design concepts and sensor fault detection algorithm using Kalman Filter. The algorithm was verified to use HILS that is composed of two FCCs, motion table, visualization system, cockpit, and flight model computer. The FCC was developed to be able to mount on small aircraft.

Keywords

References

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