Skip to Main content Skip to Navigation
Conference papers

Fault detection in flight guidance dynamics based on differential flatness

Abstract : 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.
Document type :
Conference papers
Complete list of metadatas

Cited literature [8 references]  Display  Hide  Download

https://hal-enac.archives-ouvertes.fr/hal-00938131
Contributor : Laurence Porte <>
Submitted on : Monday, June 23, 2014 - 4:44:10 PM
Last modification on : Tuesday, February 11, 2020 - 1:59:59 PM
Long-term archiving on: : Tuesday, September 23, 2014 - 10:40:21 AM

File

433.pdf
Publisher files allowed on an open archive

Identifiers

Citation

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⟩

Share

Metrics

Record views

320

Files downloads

301