Conference papers
Fault detection using differential flatness in flight guidance systems
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.
Cited literature [8 references]
https://hal-enac.archives-ouvertes.fr/hal-00938151
Contributor : Laurence Porte <>
Submitted on : Monday, June 23, 2014 - 4:14:04 PM
Last modification on : Tuesday, February 11, 2020 - 1:59:58 PM
Document(s) archivé(s) le : Tuesday, September 23, 2014 - 10:40:32 AM
Contributor : Laurence Porte <>
Submitted on : Monday, June 23, 2014 - 4:14:04 PM
Last modification on : Tuesday, February 11, 2020 - 1:59:58 PM
Document(s) archivé(s) le : Tuesday, September 23, 2014 - 10:40:32 AM
File
363.pdf
Publisher files allowed on an open archive
