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논문 기본 정보

자료유형
학술저널
저자정보
Ho-Hyun Shin (Seoul National University) Sang-Hyun Lee (Seoul National University) Youdan Kim (Seoul National University) Eung-Tae Kim (Korea Aerospace Research Institute) Ki-Jung Sung (Korea Aerospace Research Institute)
저널정보
한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.12 Number.3
발행연도
2011.9
수록면
241 - 251 (11page)

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초록· 키워드

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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.

목차

Abstract
1. Introduction
2. Flight Envelope and Loss of Control
3. Flight Envelope Protection System
4. Controller Design
5. Numerical Simulations
6. Conclusions
Acknowledgments
References

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