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Development and Validation of Automatic Thrust Control System

자동추력 제어시스템 개발 및 검증

  • 김종섭 (한국항공우주산업(주) 비행제어팀) ;
  • 조인제 (한국항공우주산업(주) T/A-50 비행제어팀) ;
  • 이동규 (한국항공우주산업(주) 비행제어팀)
  • Received : 2010.02.22
  • Accepted : 2010.07.12
  • Published : 2010.09.01

Abstract

Modern version of advanced supersonic fighter have ATCS (Automatic Thrust Control System) to maximum flight safety, fuel efficiency and mission capability the integrated advanced autopilot system such as TFS (Terrain Following System), GCAS (Ground Collision Avoidance System) and AARS (Automatic Attitude Recovery System) and etc. This paper addresses the design and verification of ATCS based on advanced supersonic trainer in HILS (Hardware In the Loop Simulator) with minimum hardware modification to reduce of development cost and maintain of system reliability. The function of ATCS is consisted of target speed hold mode in UA (Up and Away) and angle of attack hold mode in PA (Power Approach). The real-time pilot evaluation reveals that pilot workload is minimized in cruise and approach flight stage by ATCS.

Keywords

References

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