위성발사체 궤도추정을 위한 융합필터 연구

Fusion Tracking Filter for Satellite Launch Vehicles

  • 유성숙 (한국항공대학교 항공우주 및 기계공학부) ;
  • 김정래 (한국항공대학교 항공우주 및 기계공학부) ;
  • 송용규 (한국항공대학교 항공우주 및 기계공학부) ;
  • 고정환 (한국항공우주연구원)
  • 발행 : 2007.12.01

초록

The flight safety system for the satellite launch vehicles is required in order to minimize the risk due to launch vehicle failure. For prompt and reliable decision of flight termination, the flight safety system usually uses multiple sensors to estimate launch vehicle's flight trajectory. In that case, multiple types of observed tracking data makes it difficult to identify the flight termination condition. Therefore, a fusion tracking filter handling the multiple tracking data is necessary for the flight safety system. This research developed a simulation software for generating multiple types of launch vehicle tracking data, and then processed the data with fusion filters.

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