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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 OpenAlexaff
S. Mohammad Hosseini, Georges Ghazi, Ruxandra Mihaela Botez

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.

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)0.000
metaresearch head score (Gemma)0.000
Version: metacan-v3-hybrid-931329e0061cValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: none
GenreCandidate signal: Empirical · Consensus signal: none
Teacher disagreement score0.003
Threshold uncertainty score0.008

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0010.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0010.000
Open science0.0010.000
Research integrity0.0010.001
Insufficient payload (model declined to judge)0.0020.001

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 head0.028
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

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 designSimulation or modeling
Domainnot available
GenreEmpirical

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

Citations3
Published2023
Admission routes1
Has abstractyes

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