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 |
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DOIs | |
Publication status | Published - 2008 |
Event | 17th IFAC World Congress - South Korea Duration: 1 Jan 2008 → … |
Conference
Conference | 17th IFAC World Congress |
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Period | 1/01/08 → … |