Abstract

International audience; With the growth of civil aviation traffic, enhanced accuracy performances are required from guidance systems to maintain efficiency and safety in flight operations. This communication proposes a new representation of aircraft flight dynamics at approach for landing and a space-based nonlinear dynamic inversion control for a transportation aircraft. The main novelty is that the adopted independent variable is the distance to land. This new representation of flight dynamics should support the development of improved aircraft guidance systems.


Original document

The different versions of the original document can be found in:

http://dx.doi.org/10.1109/eais.2012.6232823
https://dblp.uni-trier.de/db/conf/eais/eais2012.html#BouadiM12,
https://hal-enac.archives-ouvertes.fr/hal-00938791/document,
https://academic.microsoft.com/#/detail/2064587530
https://hal-enac.archives-ouvertes.fr/hal-00938791/document,
https://hal-enac.archives-ouvertes.fr/hal-00938791/file/480.pdf
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Published on 01/01/2012

Volume 2012, 2012
DOI: 10.1109/eais.2012.6232823
Licence: CC BY-NC-SA license

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