DOI QR코드

DOI QR Code

GUI 기반 가상모의시험 비행성 평가 S/W 개발

S/W Development of Flying Qualities Evaluation in Virtual Flight Test using MATLAB GUI

  • Cho, Seung-Gyu (Department of Aerospace and System Engineering Gyeongsang National University) ;
  • Rhee, Ihn-Seok (School of Mechatronics Engineering Korea University of Technology And Education) ;
  • Kim, Byoung-Soo (Department of Aerospace and System Engineering Gyeongsang National University)
  • 투고 : 2012.09.18
  • 심사 : 2012.12.27
  • 발행 : 2013.01.01

초록

항공기 비행성 평가 과정에서는 수많은 평가의 반복이 필요하기 때문에 평가 시스템에 있어서 간결하고 명확한 응용 인터페이스가 중요하다. 본 비행성 평가 프로그램은 달라진 트림 조건의 사용자 환경과 함께 효율적인 비행성 평가 사용자 환경을 구현하였다. 그리고 14 항목으로 선별된 무인 고정익기의 비행성 평가 자동화 모듈을 모두 탑재한 종합평가 환경을 구성하였다. 이에 따라 비행제어시스템 개발은 물론 비행성이 고려된 항공기를 개발함에 있어서 검증 및 평가 과정에 소요되는 비용과 시간을 대폭 감소시키고 향후 확장성을 겸비한 유용한 시험 평가 검증 도구로 활용될 수 있을 것으로 사료된다.

In an evaluation process of aircraft flying qualities, a clear and concise application interface is important since an evaluation process requires numerous repeated evaluation. This flight evaluation program have implemented efficient flight evaluation user interface along with changed trim condition interface and composed of comprehensive evaluation interface have mounted all automated FQ evaluation modules that was selected to be compose of 14 items in respect of an unmanned fixed-wing aircraft. Accordingly when it is necessary to design the flight control system as well as to develop a FQ considered aircraft, this S/W can be utilized as a tool that is a useful test evaluation S/W with scalability and enable to reduce the time and the cost of verification and evaluation process.

키워드

참고문헌

  1. U.S. Department of Defense, Military Standard-Flying Qualities of Piloted Aircraft, MIL-HDBK-1797, 1997.
  2. Anon, Military Standard-Flying Qualities of Piloted Aircraft, MIL-STD-1797A (USAF), U.S. Department of Defense, USA, 1987.
  3. Eugene A. Morelli, "Identification of Low Order Equivalent System models From Flight Test Data," NASA/TM-2000-210117.
  4. Timothy J. Curry, "Estimation of Handling Qualities Parameters of the Tu-144 Supersonic Transport Aircraft Flight Test Data," NASA/CR-2000-210290.
  5. Engene A. "Morelli, High A.ccuracy Evaluation of the Finite Fourier Transform using Sampled Data," NASA/TM 110340.
  6. Morelli, E.A., "System IDentification Programs for AirCraft (SIDPAC)," AIAA Paper 2002-4704, AIAA Atmospheric Flight Mechanics Conference, Monterey, CA, August 2002
  7. Klein, V., Morelli, E. A., Aircraft System Identification : Theory and Practice, Reston, AIAA, 2006
  8. Jeong-ho Park, Boo-min Kim, Byoung-soo Kim, "Evaluation Technique and Automating Code Development of Handling Quality for Conventional Aircraft," KSAS Fall Conference, 2008.11
  9. Hwan-ho Jeong, Sang-Hwee Hong, Do-myoung Kim, Jinyoung Suk, "Assessment of a Longitudinal Axis Handling Qualities for Unmanned Rotorcraft Using ADS-33E,," KSAS Spring Conference, 2009.4
  10. Deok-kon Kim, Byoung-soo Kim, Choon -Bae Park, "Estimation of Handling Qualities Parameters Using Low Order Equivalent System," KSAS Fall Conference, 2002.11
  11. Youngsu Han, Youdan Kim, "UAV Performance Analysis Using Low-Order Equivalent System Identification," KSAS Fall Conference, 2005.11