Robust adaptive fault-tolerant control of the F-14 aircraft under sensor failures

Sajjad Fekri; Da-Wei Gu; Ian Postlethwaite; Michael Athans

doi:10.3182/20080706-5-KR-1001.01721

Robust adaptive fault-tolerant control of the F-14 aircraft under sensor failures

Sajjad Fekri, Da-Wei Gu, Ian Postlethwaite, Michael Athans

Research output: Contribution to conference › Paper › peer-review

5 Citations (Scopus)

Abstract

This paper presents a novel fault detection and isolation (FDI) architecture applied to the lateral-directional axis of an F-14 aircraft during powered approach to landing under sensor failures. The fault-tolerant architecture employed is based on the so-called Robust Multiple-Model Adaptive Control (RMMAC) and hence is referred to as RMMAC/FDI. The results demonstrate successful stability and performance of the RMMAC/FDI architecture

Original language	English
DOIs	https://doi.org/10.3182/20080706-5-KR-1001.01721
Publication status	Published - 2008
Event	17th IFAC World Congress - South Korea Duration: 1 Jan 2008 → …

Conference

Conference	17th IFAC World Congress
Period	1/01/08 → …

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10.3182/20080706-5-KR-1001.01721

Cite this

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abstract = "This paper presents a novel fault detection and isolation (FDI) architecture applied to the lateral-directional axis of an F-14 aircraft during powered approach to landing under sensor failures. The fault-tolerant architecture employed is based on the so-called Robust Multiple-Model Adaptive Control (RMMAC) and hence is referred to as RMMAC/FDI. The results demonstrate successful stability and performance of the RMMAC/FDI architecture",

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AU - Fekri, Sajjad

AU - Gu, Da-Wei

AU - Postlethwaite, Ian

AU - Athans, Michael

PY - 2008

Y1 - 2008

N2 - This paper presents a novel fault detection and isolation (FDI) architecture applied to the lateral-directional axis of an F-14 aircraft during powered approach to landing under sensor failures. The fault-tolerant architecture employed is based on the so-called Robust Multiple-Model Adaptive Control (RMMAC) and hence is referred to as RMMAC/FDI. The results demonstrate successful stability and performance of the RMMAC/FDI architecture

AB - This paper presents a novel fault detection and isolation (FDI) architecture applied to the lateral-directional axis of an F-14 aircraft during powered approach to landing under sensor failures. The fault-tolerant architecture employed is based on the so-called Robust Multiple-Model Adaptive Control (RMMAC) and hence is referred to as RMMAC/FDI. The results demonstrate successful stability and performance of the RMMAC/FDI architecture

UR - https://www.scopus.com/pages/publications/79961019925

U2 - 10.3182/20080706-5-KR-1001.01721

DO - 10.3182/20080706-5-KR-1001.01721

M3 - Paper

T2 - 17th IFAC World Congress

Y2 - 1 January 2008

ER -

Robust adaptive fault-tolerant control of the F-14 aircraft under sensor failures

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