International Journal of Aerospace System Engineering

  • 제3권2호
  • /
  • Pages.1-8
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  • 2016
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  • 2383-4986(pISSN)
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  • 2508-7169(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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An Investigation of the Effects of Flaperon Actuator Failure on Flight Maneuvers of a Supersonic Aircraft

  • Oh, Seyool (Aircraft Research & Development Division, Korea Aerospace Industries, ltd) ;
  • Cho, Inje (Aircraft Research & Development Division, Korea Aerospace Industries, ltd) ;
  • McLaughlin, Craig (Dept. of Aerospace Engineering, The University of Kansas)
  • 투고 : 2016.11.01
  • 심사 : 2016.12.28
  • 발행 : 2016.12.31
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초록

The improvements in high performance and agility of modern fighter aircraft have led to improvements in survivability as well. Related to these performance increases are rapid response and adequate deflection of the control surfaces. Most control surface failures result from the failure of the actuator. Therefore, the failure and behavior of the actuators are essential to both combat aircraft survivability and maneuverability. In this study, we investigate the effects of flaperon actuator failure on flight maneuvers of a supersonic aircraft. The flight maneuvers were analyzed using six degrees of freedom (6DOF) simulations. This research will contribute to improvements in the reconfiguration of control surfaces and control allocation in flight control algorithms. This paper compares the results of these 6DOF simulations with the horizontal tail actuator failures analyzed previously.

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참고문헌

  1. Seyool Oh, C.S. Lee, G.O. Koh, S.W. Kim, and I. Cho, The Effectiveness of the Actuator under Normal and Excessive State of Hinge Moment for a Supersonic Aircraft, The Korean Society for Aeronautical and Space Sciences, Jeju Island, Korea, Fall 2015.
  2. Seyool Oh, J.M. Sung, C.S. Kim, and I. Cho, Study on Advanced Control Laws for New Combat Aircraft, The Korean Society for Aeronautical and Space Sciences, Goseong-Gun, Korea, Spring 2016.
  3. E.T. Raymond, P.E. and C.C. Chenoweth, Aircraft Flight Control Actuation System Design, Society of Automotive Engineers, Inc., 1993
  4. Loss of Control In-Flight Accident Analysis Report, The International Air Transport Association (IATA) 2010-2014
  5. Jan Roskam, Airplane Flight Dynamics and Automatic Flight Control Part I, DARcorporation, 2007
  6. Seyool Oh, C.S. Kim, I. Cho, and Shawn Keshmiri, Study on Application of Control Allocation to Korean Fighter eXperimental, 2016 Asian Joint Symposium on Aerospace Engineering, Jeju Island, Korea, Spring 2016
  7. Seyool Oh, Inje Cho, and Craig McLaughlin, An Investigation of Effects of Flight Maneuvers on a Supersonic Aircraft with Horizontal Tail Actuator Failure, 30th Congress of the International Council of the Aeronautic Sciences, Daejeon, Korea, 25-30, 2016