New approach to detecting failure modes for an aircraft flight path control system

Koki Fujita, Norihiro Goto

研究成果: ジャーナルへの寄稿記事

抄録

In this paper, a new method to detect failure modes for dynamical systems is proposed, taking an aircraft flight path control system as an example. The method is based on the system identification theory to estimate the changes in dynamical properties of the system. Failure mode indices based on the robust control theory are also introduced to exhibit the nature of the failure occurring in the system. Finally, a numerical simulation is conducted to demonstrate the efficiency of the proposed method.

元の言語英語
ページ(範囲)293-303
ページ数11
ジャーナルMemoirs of the Graduate School of Engineering, Kyushu University
59
発行部数4
出版物ステータス出版済み - 12 1 1999

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Flight paths
Failure modes
control system
aircraft
flight
Aircraft
Control systems
Robust control
Control theory
Identification (control systems)
Dynamical systems
Computer simulation
simulation
method

All Science Journal Classification (ASJC) codes

  • Energy(all)
  • Process Chemistry and Technology
  • Atmospheric Science
  • Management of Technology and Innovation
  • Earth and Planetary Sciences(all)

これを引用

New approach to detecting failure modes for an aircraft flight path control system. / Fujita, Koki; Goto, Norihiro.

:: Memoirs of the Graduate School of Engineering, Kyushu University, 巻 59, 番号 4, 01.12.1999, p. 293-303.

研究成果: ジャーナルへの寄稿記事

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