MétaCan
Menu
Back to cohort
Record W4223943046 · doi:10.22215/etd/2022-14907

Modelling, Flight Dynamics and Inner-Loop Control of an Urban Air Mobility Vehicle Subject to Empirically-Developed Urban Airflow Disturbances

2022· dissertation· en· W4223943046 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

Venuenot available
Typedissertation
Languageen
FieldEngineering
TopicAerospace and Aviation Technology
Canadian institutionsCarleton University
FundersNatural Sciences and Engineering Research Council of Canada
KeywordsAirflowAerodynamicsAutopilotAir traffic controllerController (irrigation)Transport engineeringEngineeringEnvironmental scienceAir traffic controlAerospace engineeringMechanical engineering

Abstract

fetched live from OpenAlex

Advanced Air Mobility in general, and Urban Air Mobility in particular, are expected to play a significant role in improving transportation of people and goods in increasingly growing urban centres while contributing to reduction in emissions and reaching the goal of sustainable urban growth. The goal of this work was to investigate the performance of a novel controller as an autopilot for a generic aircraft operating in urban airflow. In this investigation, the extraction of geometric, inertial and aerodynamic properties of a generic urban air taxi, similar in design to the Bell Nexus 4EX, was carried out. Subsequently the properties were used as a basis for the development of a linearized flight dynamics numerical model of the aircraft. Flights about a trimmed condition at cruising speed were simulated including cases where the urban air taxi was immersed in empirically-developed urban airflow disturbances. The open-loop response of the urban air taxi was assessed and classical proportional-integral-derivative and Active Disturbance Rejection Control inner-loop controllers were developed. The performance of the controllers in presence of the aforementioned urban airflow disturbance were then examined and compared. Active Disturbance Rejection Control was shown to perform similarly to proportional-integral-derivative control in the flight of the aircraft immersed in a representative urban airflow environment. Future investigations were recommended to increase the model fidelity to understand how unsteady aerodynamics would affect the aircraft motion and that real world considerations be included to further test Active Disturbance Rejection Control.

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: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.142
Threshold uncertainty score1.000

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0010.000
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 head0.007
GPT teacher head0.231
Teacher spread0.224 · 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

Citations4
Published2022
Admission routes2
Has abstractyes

Explore more

Same topicAerospace and Aviation TechnologyFrench-language works237,207