MétaCan
Menu
Back to cohort
Record W1489535156

Méthode des impédances mécaniques virtuelles optimales pour le contrôle actif vibroacoustique d'un panneau aéronautique

2014· dissertation· fr· W1489535156 on OpenAlexfundno aff
Marc Michau

Bibliographic record

VenueHAL (Le Centre pour la Communication Scientifique Directe) · 2014
Typedissertation
Languagefr
FieldEngineering
TopicAeroelasticity and Vibration Control
Canadian institutionsnot available
FundersNatural Sciences and Engineering Research Council of CanadaSchweizerischer Nationalfonds zur Förderung der Wissenschaftlichen ForschungNational Science Foundation
KeywordsHumanitiesPhysicsPhilosophy
DOInot available

Abstract

fetched live from OpenAlex

Composite materials are widely used in the aeronautic industry for their low mass/stiffness ratio. However, this property tends to reduce the acoustic transmission loss, particularly at low frequencies. At these frequencies, active control is an effective mean of controlling sound transmission. Among the various approaches, Active Structural Acoustic Control (ASAC) has received considerable attention because transducers can be integrated to the structure. In order to reduce the acoustic power radiated by a flexible panel, dual colocated actuator sensor pairs are used to modify its vibration. The control strategy implemented for harmonic disturbances leads to locally impose a virtual mechanical impedance to the structure, using a decentralized controller. This virtual mechanical impedance is computed in order to minimise the radiated acoustic power. The challenging problem is then to find the local control to impose on each independent devices that minimizes the global acoustic radiation of the structure. The proposed approach consists in two steps : (1) the matrix of optimal virtual mechanical impedance is calculated by measuring the primary disturbance and the transfer functions between actuators and structural / acoustic sensors, (2) the virtual mechanical impedance objective is achieved using a real-time integral controller. Special focus is put on the discussion about such control approach versus a classical active damping strategy were the virtual mechanical impedance is defined as real positive. Considering that optimal control is computed during the first step for a given primary disturbance, the robustness of the method to variations of the primary disturbance between step 1 and step 2 is discussed. Theoretical and experimental results are compared in the case of a simply supported thin aluminum plate and a primary disturbance under the form of an incident plane wave. Then, the method is implemented on a curved composite aircraft panel comprising a window. Unlike most of previous studies where dissipative virtual mechanical impedance are imposed, it clearly appears that optimal control can require energy injection from the control units into the structure.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame machine prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. The Gemma side is a direct model label for every work in the frame, read from the title-only record. The Codex side is a classifier learned from the 10,348 direct Codex labels and calibrated to design-weighted sample rates; fields without enough sample support carry no Codex call. Candidate is the union of the two sides; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels.

metaresearch head score (Codex)0.001
metaresearch head score (Gemma)0.001
Version: metacan-v3-hybrid-931329e0061cValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Bench or experimental · Consensus signal: Bench or experimental
GenreCandidate signal: Methods · Consensus signal: Methods
Teacher disagreement score0.004
Threshold uncertainty score0.015

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0010.001
Meta-epidemiology (narrow)0.0010.001
Meta-epidemiology (broad)0.0010.000
Bibliometrics0.0010.000
Science and technology studies0.0000.001
Scholarly communication0.0010.001
Open science0.0010.001
Research integrity0.0010.001
Insufficient payload (model declined to judge)0.0040.001

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.012
GPT teacher head0.222
Teacher spread0.209 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one source (direct Gemma or distilled Codex), not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designBench or experimental
Domainnot available
GenreMethods

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations0
Published2014
Admission routes1
Has abstractyes

Explore more

Same venueHAL (Le Centre pour la Communication Scientifique Directe)Same topicAeroelasticity and Vibration ControlFrench-language works237,207