New approach to detecting failure modes for an aircraft flight path control system
Koki Fujita, Norihiro Goto
航行ダイナミクス
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.
Memoirs of the Graduate School of Engineering, Kyushu University
出版済み - 12 1 1999
Failure modes
Robust control
Identification (control systems)
Energy(all)
Fujita, K., & Goto, N. (1999). New approach to detecting failure modes for an aircraft flight path control system. Memoirs of the Graduate School of Engineering, Kyushu University, 59(4), 293-303.
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.
Fujita, K & Goto, N 1999, 'New approach to detecting failure modes for an aircraft flight path control system', Memoirs of the Graduate School of Engineering, Kyushu University, 巻. 59, 番号 4, pp. 293-303.
Fujita K, Goto N. New approach to detecting failure modes for an aircraft flight path control system. Memoirs of the Graduate School of Engineering, Kyushu University. 1999 12 1;59(4):293-303.
Fujita, Koki ; Goto, Norihiro. / New approach to detecting failure modes for an aircraft flight path control system. :: Memoirs of the Graduate School of Engineering, Kyushu University. 1999 ; 巻 59, 番号 4. pp. 293-303.
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title = "New approach to detecting failure modes for an aircraft flight path control system",
abstract = "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.",
author = "Koki Fujita and Norihiro Goto",
journal = "Memoirs of the Faculty of Engineering, Kyushu University",
publisher = "Kyushu University, Faculty of Science",
T1 - New approach to detecting failure modes for an aircraft flight path control system
AU - Fujita, Koki
AU - Goto, Norihiro
N2 - 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.
AB - 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.
JO - Memoirs of the Faculty of Engineering, Kyushu University
JF - Memoirs of the Faculty of Engineering, Kyushu University