Design of a Flight Envelope Protection System Using a Dynamic Trim Algorithm

  • Shin, Ho-Hyun (School of Mechanical and Aerospace Engineering, Seoul National University) ;
  • Lee, Sang-Hyun (School of Mechanical and Aerospace Engineering, Seoul National University) ;
  • Kim, You-Dan (School of Mechanical and Aerospace Engineering, Seoul National University) ;
  • Kim, Eung-Tae (Korea Aerospace Research Institute) ;
  • Sung, Ki-Jung (Korea Aerospace Research Institute)
  • 투고 : 2011.04.28
  • 심사 : 2011.07.07
  • 발행 : 2011.09.30


Most large commercial aircrafts and high performance military aircrafts use fly-by-wire (FBW) or fly-by-light systems to improve their controllability, comfort, and safety. A flight envelope protection technique is used with flight control systems utilizing the FBW technique. Such flight envelope protection systems prevent these aircraft from exceeding the structural/aerodynamic limits and control their surface limits. This is accomplished by predicting the values of the future state variables and adaptively compensating the control action. In this study, the conventional dynamic trim algorithm of the flight envelope protection is modified to increase the method accuracy and to handle cases with multiple variables. Numerical simulation is also performed to verify the performance of the proposed method.


연구 과제 주관 기관 : National Research Foundation of Korea (NRF)


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