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ADS-33 평가기준에 따른 소방헬기 비행시뮬레이터의 비행조종성 예비평가

Preliminary Evaluation of Handling Qualities of a SAR(Search & Rescue) Helicopter Simulator Based on ADS-33 Requirements

  • 투고 : 2016.04.26
  • 심사 : 2016.08.18
  • 발행 : 2016.09.01

초록

본 연구는 헬리콥터 비행 시뮬레이터 개발의 첫 번째 단계의 일환으로 비행 운동 모델의 비행조종성을 해석적으로 평가한다. 비행 운동 모델은 시뮬레이터의 목표 항공기인 AS365 N2의 공개 정보를 사용하여 생성하였다. 해당 비행 시뮬레이터는 소방 임무에 대한 조종사 교육 및 연구 도구로 개발 중이다. 모델의 평가는 비행 시험 데이터를 통한 검증이 이루어지기 전에 모델의 비행 특성과 다음 개발 단계로의 적합성을 평가하기 위하여 수행된다. 평가는 항공기분류, 임무 및 환경을 고려하여 ADS-33E-PRF(Aeroautical Design Standard Performance Specification Handling Qualities Requirement)의 기준에 의거하여 수행한다. 항공기의 해석적 비행은 규정에 대한 적합성 평가를 위해 요구되는 혹은 권장되는 비행시험절차를 따른다. 평가 결과는 ADS-33E-PRF에 명시된 조종성 등급에 따라 평가되는데 RotorLibFDM을 기반으로 생성된 비행 운동 모델이 헬기 비행에 대한 기본 교육과 연구로 사용될 수 있는 일반적인 헬리콥터 시뮬레이터에 대한 만족스러운 플랫폼을 제공함이 확인되었다.

As a part of the first stage in the helicopter flight simulator development, this study numerically evaluates handling qualities of the dynamics model. The flight dynamics model was generated using public information for AS365 N2, the target aircraft of the simulator. The flight simulator is under development as a pilot training and research tool for firefighting missions. The assessment of the model intends to validate general characteristics and suitability before the model is enhanced with flight test data. The evaluation is based on the ADS-33E-PRF(Aeroautical Design Standard Performance Specification Handling Qualities Requirement) criteria, with consideration of category of the aircraft, missions, and environment. The numerical operations follow required or recommended procedures of flight test for compliance demonstration. Evaluation results are evaluated according to the rating specified in maneuverability ADS-33E-PRF. Results have identified to provide a satisfactory platform for flight dynamic model in the general helicopter simulator generated based on the RotorLibFDM, and can be used as a base for basic training and research.

키워드

참고문헌

  1. Thaddeus T. Kaplita, Joseph T. Driscoll, Myron A. Difler, and Steven W. Hong, "Helicopter Simulation Development by Correlation with Frequency Sweep Flight Test Data", 45th Annual Forum, Boston, MA, May 22-24, 1989, pp. 681-692.
  2. Jurgen Kaletka and Wolfgang von Grunhagen, "Identification of Mathematical Derivative Models for the Design of a Model Following Control System", 45th Annual Forum, Boston, MA, May 22-24, 1989, pp. 656-668.
  3. Mark D. White and Gareth D. Padfield, "The Use of Flight Simulation for Research and Teaching in Academia", AIAA Atmospheric Flight Mechanics Conference and Exhibit, Keystone, Colorado, 21 - 24 August 2006.
  4. Peter H. Zipfel, "Modeling and Simulation of Aerospace Vehicle Dynamics", AIAA Education Series, 2000.
  5. Heinz-Jurgen Pausder and Chris L. Blanken, "Investigation of the Effects of Bandwidth and Time Delay on Helicopter Roll-Axis Handling Qualities", 18th European Rotorcraft Forum, Avignon, France, September 1992.
  6. Advanced Rotorcraft Technology, Inc., "FLIGHTLAB Theory Manual", April 2001.
  7. RTDynamics, "RotorLibFDM: A Helicopter Dynamics Simulation Library", http://www.rtdynamics.de/Public/Showcase/Whitepaper_RotorLib_FDM.pdf.
  8. "Aeronautical Design Standard Performance Specification Handling Qualities Requirements for Military Rotorcraft", ADS-33E-PRF, 21 March 2000.
  9. Mark B. Tischler, Christina M. Ivler, M. Hossein Mansur, Kenny K. Cheung, Tom Berger, and Marcos Berrios, "Handling- Qualities Optimization and Trade-offs in Rotorcraft Flight Control Design", The RAeS Rotorcraft Handling-Qualities Conference, University of Liverpool, U.K., 4-6 Nov 2008.
  10. Carlo A. Gerboni, Stefano Geluardi, Mario Olivari, Frank M. Nieuwenhuizen, Heinrich H. Bulthoff, and Lorenzo Pollini, "Development of a 6 DoF Nonlinear Helicopter Model for the MPI Cybermotion Simulator", 40th European Rotorcraft Forum, Curran, Red Hook, NY, USA, July 2015, pp. 615-626.
  11. Luigi S. Cicolani, Allen H. McCoy, Ranjana Sahai, Peter H. Tyson, Mark B. Tischler, Aviv Rosen, and George E. Tucker, "Flight Test Identification and Simulation of a UH-60A Helicopter and Slung Load", Journal of American Helicopter Society, Volume 46, Number 2, 1 April 2001, pp. 140-160. https://doi.org/10.4050/JAHS.46.140
  12. David G. Mitchell, David J. Moorhouse, David B. Doman, David H. Mason, David L. Key, David L. Raney, David H. Klyde, David K. Schmidt, and David B. Leggett, "The Evolution, Revolution, and Challenges of Handling Qualities", AIAA Atmospheric Flight Mechanics Conference and Exhibit, Austin, Texas, 11-14 August 2003.
  13. Gareth D. Padfield, "Helicopter Flight Dynamics: The Theory and Application of Flying Qualities and Simulation Modeling", AIAA Education Series, 1996.
  14. Jeffery N. Williams, Johnnie A. Ham, and Mark B. Tischler, "FLIGHT TEST MANUAL-Rotorcraft Frequency Domain Flight Testing", AQTD Project No. 93-14, 1995.
  15. Chris L. Blanken, Roger H. Hoh, David G. Mitchell, and David L. Key, "Test Guide for ADS-33E-PRF", Special Report AMR-AF-08-07, July2008.
  16. Mark. B. Tischler, Jay W. Fletcher, Vernon L. Diekrnann, Robert A. Williams, and Randall W. Cason, "Demonstration of frequency-sweep testing technique using a Bell 214-ST helicopter", NASA Technical Memorandum 89422, MAY 1987.
  17. Donald T. Ward, "Introduction to Flight Test Engineering", Elsevier Science Publishers B.V., 1993.
  18. Paul Jackson, Kenneth Munson, "Jane's All the World's Aircraft 2008-2009", Jane's Information Group Limited, 2008.