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Flight control system design of UAV with wing incidence angle simultaneously and stochastically varied
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Flight control system design of UAV with wing incidence angle simultaneously and stochastically varied
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Journal Article
Flight control system design of UAV with wing incidence angle simultaneously and stochastically varied
2024
Overview
Purpose
This study aims to simultaneously and stochastically maximize autonomous flight performance of a variable wing incidence angle having an unmanned aerial vehicle (UAV) and its flight control system (FCS) design.
Design/methodology/approach
A small UAV is produced in Iskenderun Technical University Drone Laboratory. Its wing incidence angle is able to change before UAV flight. FCS parameters and wing incidence angle are simultaneously and stochastically designed to maximize autonomous flight performance using an optimization method named simultaneous perturbation stochastic approximation. Obtained results are also benefitted during UAV flight simulations.
Findings
Applying simultaneous and stochastic design approach for a UAV having passively morphing wing incidence angle and its flight control system, autonomous flight performance is maximized.
Research limitations/implications
Permission of the Directorate General of Civil Aviation in Turkish Republic is necessary for real-time flights.
Practical implications
Simultaneous stochastic variable wing incidence angle having UAV and its flight control system design approach is so useful for maximizing UAV autonomous flight performance.
Social implications
Simultaneous stochastic variable wing incidence angle having UAV and its flight control system design methodology succeeds confidence, excellent autonomous performance index and practical service interests of UAV users.
Originality/value
Creating an innovative method to recover autonomous flight performance of a UAV and generating an innovative procedure carrying out simultaneous stochastic variable wing incidence angle having UAV and its flight control system design idea.
Publisher
Emerald Publishing Limited,Emerald Group Publishing Limited
