Results 1 to 10 of about 6,396 (161)
Monitoring of a Highly Flexible Aircraft Model Wing Using Time-Expanded Phase-Sensitive OTDR [PDF]
Sensors, 2021 In recent years, the use of highly flexible wings in aerial vehicles (e.g., aircraft or drones) has been attracting increasing interest, as they are lightweight, which can improve fuel-efficiency and distinct flight performances.
Miguel Soriano-Amat +7 more
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Comprehensive Engineering Frequency Domain Analysis and Vibration Suppression of Flexible Aircraft Based on Active Disturbance Rejection Controller [PDF]
Sensors, 2022 The crash of an aircraft with an almost vertical attitude in Wuzhou, Guangxi, China, on 21 March 2022, has caused a robust discussion in the civil aviation community.
Litao Liu, Bingwei Tian
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Equivalent dynamic modeling of flexible morphing aircraft [PDF]
Science Progress, 2021 A morphing aircraft can maintain optimal flight performance by adaptively changing shape. However, large deformation and fast motion of aircraft modules lead to complicated dynamics during morphing process.
Changzhu Wei +3 more
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Modelling framework for flight dynamics of flexible aircraft
Aviation, 2016 The flight dynamics and handling qualities of any flexible aircraft can be analysed within the Cranfield Aircraft Accelerated Loads Model (CA2LM) framework. The modelling techniques and methods used to develop the framework are presented. The aerodynamic
Vilius Portapas +2 more
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AI-Enabled Flexible Sensing Skin for Next-Generation Aircraft: Toward Embodied Intelligence [PDF]
ResearchAircraft serve as the intelligent extension of human capabilities into 3-dimensional space. Next-generation aircraft will transcend the limitations of traditional fixed aerodynamic configurations, evolving into embodied intelligent agents capable of ...
JingJing Ji +5 more
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On the necessity of flexible modelling in fault detection for a flexible aircraft
IFAC-PapersOnLine, 2021 Bela Takarics, Balint Vanek
exaly +4 more sources
Aerospace, 2021 This paper focuses on the development of an explicit finite difference numerical method for approximating the solution of the inhomogeneous fourth-order Euler–Bernoulli beam bending equation with velocity-dependent damping and second moment of area, mass
Dominique Fleischmann +1 more
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A Study on Stability Boundary of Highly Flexible Aircraft With Saturation Constraint
IEEE Access, 2021 This paper deals with investigating the closed-loop stability boundary of the highly flexible aircraft with structural flexibility and input saturation constraint.
Liang Xu, Rui Cao, Yanbin Liu, Yuping Lu
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A method for flexible aircraft LFT modelling [PDF]
2009 European Control Conference (ECC), 2009 This paper presents a method to obtain a Linear Fractional Transformation (LFT) model from a set of numerical flexible aircraft models. The core of the method lies in a polynomial interpolation, but before this step, some cautious treatments must be applied to the numerical models for them to be interpolable.
Jose Torralba +3 more
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Applied Sciences, 2022 This paper makes use of sloshing reduced-order models to investigate the effects of sloshing dynamics on aeroelastic stability and response of flying wing structure.
Marco Pizzoli +2 more
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