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Record W2136059142 · doi:10.2514/6.2007-1773

Intelligent Identification System with Applications to Transient Aeroelastic Data

2007· article· en· W2136059142 on OpenAlex

Why this work is in the frame

A frame that forgets how it found something cannot be audited. These are the routes that admitted this work.

affAt least one author lists a Canadian institution in the pinned OpenAlex snapshot.
fundA Canadian funder is recorded on the work.

Bibliographic record

Venue48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference · 2007
Typearticle
Languageen
FieldEngineering
TopicAeroelasticity and Vibration Control
Canadian institutionsUniversity of Alberta
FundersMcGill UniversityTexas A and M University
KeywordsAeroelasticityTransient (computer programming)Identification (biology)Computer scienceSystem identificationControl engineeringAerodynamicsAerospace engineeringEngineeringData modelingDatabase

Abstract

fetched live from OpenAlex

In recent years, intelligent systems have become popular tools in dealing with practical problems in science and engineering. In aeroelasticity applications, a key step in developing a robust intelligent system is to construct an appropriate mathematical model which reproduces the important features of the aeroelastic system. Structural nonlinearity in aeroelasticity can be classied as dieren tiable (such as polynomial spring) or piecewise dieren tiable (such as freeplay). The corresponding mathematical models are completely dieren t, the former is a truly nonlinear system, and the later can be described by three linear systems according to the locations of the switching points. Hence, identifying the specic type of structural nonlinearity is an important component for an intelligent system. Given a transient data arising from an aeroelastic system with structural nonlinearity, this paper rst discusses the following questions: 1) how to detect the existence of the nonlinearity, 2) how to determine the specic type of structural nonlinearity, and 3) how to estimate the switching points for a freeplay model. In the second part of the present paper, we present a Kalman-based approach for the system identication. For a freeplay aeroelastic system, the Expectation Maximization algorithm and the linear Kalman lter are used to estimate the system parameters. For an aeroelastic model with polynomial nonlinearity, the extended Kalman lter or the unscented lter must be employed. Finally, we demonstrate that the developed intelligent system can be used to accurately predict the asymptotic state of a nonlinear aeroelastic system. Results obtained using wind-tunnel experimental transient data are reported.

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.

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesMeta-epidemiology (narrow)
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Theoretical or conceptual · Consensus signal: none
GenreCandidate signal: Empirical · Consensus signal: none
Teacher disagreement score0.669
Threshold uncertainty score1.000

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0010.001
Meta-epidemiology (broad)0.0010.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0010.001
Open science0.0010.000
Research integrity0.0000.000
Insufficient payload (model declined to judge)0.0000.000

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 head0.017
GPT teacher head0.240
Teacher spread0.223 · 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