Design of a supervised flight control system for aircraft relative guidance

Thierry Miquel; Felix Mora-Camino; Jean-Marc Loscos; Karim Achaibou

doi:10.1109/DASC.2003.1245845

Design of a supervised flight control system for aircraft relative guidance

Thierry Miquel ^{1, 2} Felix Mora-Camino ³ Jean-Marc Loscos ¹ Karim Achaibou ³

1 DGAC - Direction Générale de l'Aviation Civile

2 LAAS - Laboratoire d'analyse et d'architecture des systèmes

3 LAAS-DISCO - Équipe DIagnostic, Supervision et COnduite

LAAS - Laboratoire d'analyse et d'architecture des systèmes

Abstract : In this paper, the automation of the relative guidance is performed thanks to the recursive non-linear control technique, namely backstepping according to M. Krstic et al. (1995). This is quite new design methodology for construction of both feedback control laws and associated Lyapunov functions in a systematic manner. In order to tackle safety and passenger comfort aspects, which are crucial points for commercial aircraft, the controller is supervised: the purpose of this device is to handle on-line the gain of the controller, taking into account the current value of the state in order to satisfy some limitations in commercial aircraft maneuvering capabilities.

Document type :

Conference papers

Domain :

Engineering Sciences [physics] / Automatic

Complete list of metadatas

https://hal-enac.archives-ouvertes.fr/hal-00938057
Contributor : Laurence Porte <>
Submitted on : Tuesday, May 27, 2014 - 4:26:48 PM
Last modification on : Friday, January 10, 2020 - 9:10:11 PM
Long-term archiving on: Wednesday, August 27, 2014 - 10:37:33 AM

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