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Communication Dans Un Congrès Année : 2006

Fault detection in flight guidance dynamics based on differential flatness

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Résumé

In this paper, flight guidance dynamics are shown to be implicit differentially flat with respect to the inertial position of an aircraft. This proves the existence of a set of relations between these flat outputs and the state variables representative of flight guidance dynamics and between these flat outputs and the basic inputs to flight guidance dynamics. A neural network is introduced to obtain, from the actual trajectory, nominal flight parameters which can be compared with actual values to detect abnormal behaviour.
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Dates et versions

hal-00938131 , version 1 (23-06-2014)

Identifiants

Citer

Rabah Fellouah, Wen Chi Lu, Felix Mora-Camino, Andrei Doncescu. Fault detection in flight guidance dynamics based on differential flatness. DASC 2006, 25th IEEE/AIAA Digital Avionics Systerms Conference, Oct 2006, Portsmouth, United States. pp 1-8, ⟨10.1109/DASC.2006.313721⟩. ⟨hal-00938131⟩
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