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Record W4380049541 · doi:10.2514/6.2023-3802

Design of a Type Two Fuzzy-based system to Control the Pitch Rate of the Cessna Citation X

2023· article· en· W4380049541 on OpenAlex
S. Mohammad Hosseini, Georges Ghazi, Ruxandra Mihaela Botez

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.

Bibliographic record

Venuenot available
Typearticle
Languageen
FieldEngineering
TopicAdaptive Control of Nonlinear Systems
Canadian institutionsÉcole de Technologie Supérieure
Fundersnot available
KeywordsRobustness (evolution)Control theory (sociology)Fuzzy logicAvionicsSliding mode controlControl engineeringFuzzy control systemFlight simulatorComputer scienceControl systemEngineeringRobust controlSimulationAerospace engineeringNonlinear systemControl (management)Artificial intelligence

Abstract

fetched live from OpenAlex

View Video Presentation: https://doi.org/10.2514/6.2023-3802.vid In this research, a novel control methodology developed at the Laboratory of Applied Research in Active Controls, Avionics and AeroServoElasticity (LARCASE) based on a Type Two Adaptive Fuzzy Sliding Mode control system to control the pitch rate of the Cessna Citation X aircraft is presented. For this purpose, a simulation platform developed at LARCASE was used to simulate the non-linear behavior of the Cessna Citation X aircraft. This platform was designed using flight data obtained from a Research Aircraft Flight Simulator (RAFS) manufactured by CAE Inc. and which has a Level D qualification for its flight dynamics and propulsion model. According to the Federal Aviation Administration (FAA), this is the highest level of qualification for flight simulators. This study aims to design a controller that can satisfy pitch rate tracking performance. Hence, Type Two Adaptive Fuzzy Sliding Mode Control (T2AFSMC) is suggested for this application to combine the robustness of Sliding Mode Control (SMC) with the flexibility of Type Two Fuzzy Logic Control (T2FLC). Traditional SMC has some limitations in dealing with uncertainties, nonlinearities, and disturbances in complex systems. Therefore, a Type Two Fuzzy Logic System is used to approximate the unknown dynamics of the aircraft while the sliding mode controller drives the aircraft to its desired state. In addition, some adaptation laws are employed to tune the parameters of the Type Two Fuzzy System during the simulation period. Finally, the simulation outputs demonstrate the effectiveness of the T2AFSMC in achieving good tracking performance and robustness in controlling the pitch rate of the Cessna Citation X aircraft as a complex system.

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)0.001
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: none
Teacher disagreement score0.844
Threshold uncertainty score0.224

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0010.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.001
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0000.000
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 head0.028
GPT teacher head0.242
Teacher spread0.214 · 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

Quick stats

Citations3
Published2023
Admission routes1
Has abstractyes

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