Zobrazeno 1 - 10
of 36
pro vyhledávání: '"Boris Moulin"'
Publikováno v:
Journal of Guidance, Control, and Dynamics. 35:1377-1390
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0bc209f524e6e22d9c3243e9704c0034
https://doi.org/10.2514/1.56790
https://doi.org/10.2514/1.56790
Publikováno v:
Journal of Guidance, Control, and Dynamics. 33:862-872
In this paper, an adaptive feedforward control framework is proposed for the suppression of aircraft structural vibrations induced by gust perturbations to increase the resilience of the !ight control law in the presence of the aeroelastic/aeroservoe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a104cb8e71268921c62f6ba2f7b7bf0
https://doi.org/10.2514/1.46091
https://doi.org/10.2514/1.46091
Autor:
Boris Moulin
Publikováno v:
Journal of Guidance, Control, and Dynamics. 30:1367-1377
High-order quasi-linearization procedures were developed for identification of nonlinear dynamic systems modeled by a parameter-dependent linear-fractional transformation containing a linear dynamic system in the feedforward pass and a static nonline
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d6ae938fa8c6e1fbf444f6885a562940
https://doi.org/10.2514/1.27652
https://doi.org/10.2514/1.27652
Autor:
Boris Moulin, Moti Karpel
Publikováno v:
Journal of Aircraft. 44:17-25
Control laws are designed for the alleviation of dynamic gust loads on a wind-tunnel model of a transport aircraft using wing-mounted control surfaces. Three different control surfaces are used: the symmetrically actuated main ailerons, special under
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4914c7b12778c1dfa0ff1cfe83b4f81
https://doi.org/10.2514/1.19876
https://doi.org/10.2514/1.19876
Publikováno v:
Journal of Vibration and Acoustics. 129:73-83
A way to shorten the repeated analysis process is by modal coupling of the modal properties of several substructures. The main difficulty of the classical modal-coupling approach is that the modes of freeboundary structural components normally do not
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8dc764ddfe3dc770577bf4a4e17d6643
https://doi.org/10.1115/1.2202156
https://doi.org/10.1115/1.2202156
Publikováno v:
Journal of Aircraft. 42:1264-1272
Frequency-domain and time-domain approaches to dynamic response analysis of aeroservoelastic systems to atmospheric gust excitations are presented. The discrete and continuous gust inputs are defined in either time-domain or stochastic terms. The var
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e284c8ffc66577a6de346cb3417337b6
https://doi.org/10.2514/1.6678
https://doi.org/10.2514/1.6678
Publikováno v:
Journal of Aircraft. 40:946-954
An aeroservoelastic analysis procedure has been integrated with structural optimization and robust-control design tools. The multidisciplinary analysis and design process can address structural constraints, performance, and robust aeroservoelastic st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bbc9538c2cf6a04485f65673b1991a87
https://doi.org/10.2514/2.6871
https://doi.org/10.2514/2.6871
Publikováno v:
Journal of Guidance, Control, and Dynamics. 25:152-159
The procedure for structural and robust control design of multi-input/multi-output aeroservoelastic systems presented contains modeling of uncertainties, synthesis of a robust controller, and a unified structural and control optimization process unde
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c4df7557d606e05541f234aac3909e12
https://doi.org/10.2514/2.4860
https://doi.org/10.2514/2.4860
Publikováno v:
AIAA Journal. 37:1514-1519
Recent developments of the modal-based aeroelastic optimization approach facilitated efficient treatment of static-aeroelastic and stress constraints. The reduced-size models use low-frequency normal modes of the baseline structure as fixed generaliz
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a1fb93d89fa38120b07c5e586e3d0649
https://doi.org/10.2514/3.14350
https://doi.org/10.2514/3.14350
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
This paper introduces an experimental model based feedback control (EMBFC) framework for flutter suppression and gust load alleviation (GLA). The resilience of the flight control law in the presence of aeroelastic/aeroservoelastic (AE/ASE) interactio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df5c2b0610183e71e458c5fddf011b9c
https://doi.org/10.2514/6.2011-6370
https://doi.org/10.2514/6.2011-6370