Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Serge Laporte"'
Publikováno v:
Journal of Aircraft. :1-12
This paper deals with an optimal control approach for commercial aircraft trajectory planning, focusing on the vertical path and the minimization of the fuel burned. The main contribution is the optimization of the whole trajectory, also called the m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a4092cce65be8151542e5d2a3033235
https://doi.org/10.2514/1.c036784
https://doi.org/10.2514/1.c036784
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems
IEEE Transactions on Aerospace and Electronic Systems, Institute of Electrical and Electronics Engineers, 2015, 51 (4), pp.3415-3426. ⟨10.1109/TAES.2015.140309⟩
IEEE Transactions on Aerospace and Electronic Systems, 2015, 51 (4), pp.3415-3426. ⟨10.1109/TAES.2015.140309⟩
IEEE Transactions on Aerospace and Electronic Systems, Institute of Electrical and Electronics Engineers, 2015, 51 (4), pp.3415-3426. ⟨10.1109/TAES.2015.140309⟩
IEEE Transactions on Aerospace and Electronic Systems, 2015, 51 (4), pp.3415-3426. ⟨10.1109/TAES.2015.140309⟩
This study proposes a methodology that reduces the memory size of hierarchical multilevel embedded models while keeping its structure and satisfying constraints on accuracy and computation time. Based on a choice among surrogates (high dimensional mo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c9048268d2d1f425a124230211540be0
https://hal.archives-ouvertes.fr/hal-01785618
https://hal.archives-ouvertes.fr/hal-01785618
Publikováno v:
Computational Methods in Applied Sciences ISBN: 9783319115405
The objective of this study is to propose a methodology which aims at reducing the memory size of hierarchical multilevel models while satisfying both a given accuracy and a maximum computational time, and keeping the initial multilevel structure. In
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c2cd46a382b1f8ba1b750c4de6db1c97
https://doi.org/10.1007/978-3-319-11541-2_6
https://doi.org/10.1007/978-3-319-11541-2_6
Publikováno v:
10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference.
Aircraft Maximum TOW (Takeo Weight) is calculated on the SID (Standard Instrument Departure) in the case of a engine failure, so as to respect regulatory constraints. In case of mountainous landscape, a alternative trajectory can be design to reduce
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0a316952da15dae505c71f92f2b554b
https://doi.org/10.2514/6.2010-9013
https://doi.org/10.2514/6.2010-9013
Publikováno v:
9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO).
Before take-o, Airlines have to make decisions concerning payload sales at predefined time steps. These decisions may depend on uncertain time-evolutive meteorological forecasts. Therefore the payload sale strategy can be viewed as a sequential decis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b56ca276af2d2d833bb066b2da3ef27
https://doi.org/10.2514/6.2009-6946
https://doi.org/10.2514/6.2009-6946