Zobrazeno 1 - 10
of 50
pro vyhledávání: '"Martin J. Brenner"'
Publikováno v:
Journal of aircraft. 54(4)
This paper presents a model order reduction framework to construct linear parameter-varying reduced-order models of flexible aircraft for aeroservoelasticity analysis and control synthesis in broad two-dimensional flight parameter space. Genetic algo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6c9d79ec807e03efc4fb793b5e2d8da7
https://pubmed.ncbi.nlm.nih.gov/29459816
https://pubmed.ncbi.nlm.nih.gov/29459816
Publikováno v:
2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents a data analysis and modeling framework to tailor and develop linear parameter-varying (LPV) aeroservoelastic (ASE) model database for flexible aircrafts in broad 2D flight parameter space. The Kriging surrogate model is constructe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c993b70fbbd720f9c765b5e3876ce63e
https://doi.org/10.2514/6.2018-1210
https://doi.org/10.2514/6.2018-1210
Publikováno v:
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents a methodology for automated model order reduction (MOR) of flexible aircrafts to construct linear parameter-varying (LPV) reduced order models (ROM) for aeroservoelasticity (ASE) analysis and control synthesis in broad flight para
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d1833777ff8c8ed0ec17ae12ddb2bad
https://doi.org/10.2514/6.2017-1598
https://doi.org/10.2514/6.2017-1598
Aircraft structures have varying stiffness levels making them flexible. Consequently, this elastic property becomes increasingly important at high speeds affecting the flight dynamics of the aircraft. In high speed aircraft such as the F/A-18, elasti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d4a718b8a57848b440f8d77096ae101d
https://doi.org/10.15368/theses.2011.43
https://doi.org/10.15368/theses.2011.43
Publikováno v:
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
This paper presents a holistic model order reduction (MOR) methodology and framework that integrates key technological elements of sequential model reduction, consistent model representation, and model interpolation for constructing high-quality line
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e97ac122008ed2cb03d98a4be13b907
https://doi.org/10.2514/6.2016-1222
https://doi.org/10.2514/6.2016-1222
Publikováno v:
Journal of Guidance, Control, and Dynamics. 35:1169-1177
Anovel subspace system identificationmethod based on covariance estimates and inspired by classical realization techniques is presented that constructs system estimates frommeasured input–output data. The resulting algorithm allows for the identifi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de21b4252ae9da684680f07085778ab2
https://doi.org/10.2514/1.55770
https://doi.org/10.2514/1.55770
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
Publikováno v:
Journal of Guidance, Control, and Dynamics. 31:1634-1643
In this work, an aeroelastic prediction framework is formulated by blending control-oriented techniques that consist of linear fractional transformation representation, identification of nonlinear operators, and stability boundary prediction for both
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e8b65172811105cbd90394ab7d856ba
https://doi.org/10.2514/1.36117
https://doi.org/10.2514/1.36117
Autor:
Sunil L. Kukreja, Martin J. Brenner
Publikováno v:
Journal of Guidance, Control, and Dynamics. 30:557-564
Structure detection is a procedure for selecting a subset of candidate terms, from a full model description, that best describes the observed output. This is a necessary procedure to compute an efficient system description which may afford greater in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de0fc297d9a3bdfee39ee9bc3448a6c0
https://doi.org/10.2514/1.20835
https://doi.org/10.2514/1.20835
Publikováno v:
Journal of Aircraft. 44:149-162
This paper investigates the modeling of parameter-varying nonlinear aeroelastic systems using Volterra theory. With this approach, the system dynamics are expressed in terms of a set of Volterra kernels. It is well known that the parameters of aeroel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bcd8fe2c90dca8cada7a75b0732a43f0
https://doi.org/10.2514/1.22764
https://doi.org/10.2514/1.22764