• Title/Summary/Keyword: Automatic Terrain Following Simulator

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Development of Automatic Terrain Following Simulator Using Digital Terrain Elevation Data (디지털 지형 고도 데이터를 이용한 자동 지형 추종 시뮬레이터 개발)

  • Jisu Lee;MunGyou Yoo;Hyunju Lee;Ki Hoon Song;Dong-Ik Cheon;Sangchul Lee
    • Journal of Aerospace System Engineering
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    • v.18 no.1
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    • pp.88-98
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    • 2024
  • In this paper, an Automatic Terrain Following (ATF) Simulator using Digital Terrain Elevation Data (DTED) was proposed. This ATF Simulator consists of a Flight Simulator, a Radar Simulator, and a Terrain Following Computer (TFC) Simulator. DTED and radar scan data generated with DTED were used as the terrain information necessary for terrain following. The ATF Simulator provides three modes of operation: a passive mode that uses DTED, an active mode that uses radar scan data, and a hybrid mode that uses both. We developed an ATF Simulator that could reduce the cost and time required to develop a terrain following system using the LabVIEW development environment and the MATLAB App Designer development environment. It was verified by confirming that the ATF Simulator met all functional requirements.

Development and Validation of Automatic Thrust Control System (자동추력 제어시스템 개발 및 검증)

  • Kim, Chong-Sup;Cho, In-Je;Lee, Dong-Kyu
    • Journal of Institute of Control, Robotics and Systems
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    • v.16 no.9
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    • pp.905-912
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    • 2010
  • 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.