Object structure

Creator:

Edwards, Christopher ; Alwi, Halim ; Tan, Chee Pin

Contributor:

Korbicz, Józef - red. ; Uciński, Dariusz - red.

Title:

Sliding mode methods for fault detection and fault tolerant control with application to aerospace systems

Group publication title:

AMCS, Volume 22 (2012)

Subject and Keywords:

sliding modes ; fault detection ; fault tolerant control ; control allocation

Abstract:

Sliding mode methods have been historically studied because of their strong robustness properties with regard to a certain class of uncertainty, achieved by employing nonlinear control/injection signals to force the system trajectories to attain in finite time a motion along a surface in the state-space. This paper will consider how these ideas can be exploited for fault detection (specifically fault signal estimation) and subsequently fault tolerant control. ; It will also describe applications of these ideas to aerospace systems, including piloted flight simulator results associated with the GARTEUR AG16 Action Group on Fault Tolerant Control. The results demonstrate a successful real-time implementation of the proposed fault tolerant control scheme on a motion flight simulator configured to represent the post-failure EL-AL aircraft.

Publisher:

Zielona Góra: Uniwersytet Zielonogórski

Date:

2012

Resource Type:

artykuł

DOI:

10.2478/v10006-012-0008-7

Pages:

109-124

Source:

AMCS, Volume 22, Number 1 (2012) ; click here to follow the link

Language:

eng

Rights:

Biblioteka Uniwersytetu Zielonogórskiego