Recently, Korea Air Force has been facing a lot of problems in its pilot training system such as training time shortage due to the expensive gas price, noise pollution and difficulties in finding airspace for training. To tackle these problems, a new training system (called L-V training system) using both aircraft and its simulator has been suggested. In the system, a data link is established between aircraft and simulator to exchange their flight information. Using the flight information of simulator, aircraft can perform various air missions with or against imaginary aircraft (i.e., simulator). For this system, it is crucially important that fair fighting condition has to be guaranteed between aircraft and simulator. In this paper, we suggested an approach to impose a maneuvering restriction to simulator in order to provide fair fighting condition between aircraft and simulator.

1. 서 론
 2. 전투기 조종사의 중력가속도 내성 연구
  2.1 중력가속도 내성 측정 방법
  2.2 중력가속도 내성 소모율, 회복율 및 균형 중력가속도
  2.3 관련 연구
 3. 실험장비 및 실험 절차
  3.1 실험장비
  3.2 실험대상자 및 절차
  3.3 중력가속도 내성 소모율 측정
  3.4 중력가속도 내성 회복율 측정
  3.5 균형 중력가속도 측정
 4. 실험결과 및 분석
  4.1 중력가속도 내성 소모율
  4.2 중력가속도 내성 회복율
  4.3 균형 중력가속도
 5. 시뮬레이터 기동제한 프로그램 구현
 6. 결 론
 Acknowledgement
 References

• 박명환(공군사관학교) | Myunghwan Park
• 유승훈(공군사관학교) | Seunghoon Yoo
• 설현주(공군사관학교) | Hyeonju Seol Corresponding Author
• 김천영(국방과학연구소) | Cheonyoung Kim
• 홍영석(국방과학연구소) | Youngseok Hong