Skip to Main content Skip to Navigation
Conference papers

Generic 4D flight guidance based on differential flatness

Abstract : With the increase of traffic density, it appears of interest to design more versatile guidance systems for civil transportation aircraft. In this paper, a new approach is proposed to design a guidance system able to achieve 4D trajectory tracking. Flight guidance dynamics are shown to be implicit differentially flat with respect to the inertial position of an aircraft. To overcome the numerical difficulty implied by this implicit property, artificial neural networks are introduced to capture the differential relationship between guidance parameters and attitude control inputs. A corrective term is also introduced to take into account the effects of model approximation, neural network errors and disturbances.
Document type :
Conference papers
Complete list of metadatas

Cited literature [6 references]  Display  Hide  Download

https://hal-enac.archives-ouvertes.fr/hal-00938155
Contributor : Laurence Porte <>
Submitted on : Tuesday, May 27, 2014 - 5:03:28 PM
Last modification on : Tuesday, October 27, 2020 - 1:14:01 PM
Long-term archiving on: : Wednesday, August 27, 2014 - 10:38:08 AM

File

Miquel_ACA2007.pdf
Files produced by the author(s)

Identifiers

Citation

Wen Chi Lu, Lili Duan, Thierry Miquel, Felix Mora-Camino. Generic 4D flight guidance based on differential flatness. ACA 2007, 17th IFAC Symposium on Automatic Control in Aerospace, Jun 2007, Toulouse, France. pp 353-358, ⟨10.3182/20070625-5-FR-2916.00061⟩. ⟨hal-00938155⟩

Share

Metrics

Record views

369

Files downloads

452