Results 11 to 20 of about 24,098 (229)
IEEE Access, 2018 Flight performance calculation is an important part of the micro flapping wing air vehicle design. It is used to verify whether the air vehicle design meets the performance requirements so as to make targeted improvements to the design.
Jianlin Xuan, Z. Yang, P. Nian, D. Ma
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Neurobiologically Inspired Control of Engineered Flapping Flight [PDF]
, 2009 This article presents a new control approach for engineered flapping flight with many interacting degrees of freedom. This paper explores the applications of neurobiologically inspired control systems in the form of Central Pattern Generators (CPG) to
Chung, Soon-Jo +2 more
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Mechanism and Kinematics for Flapping Wing Micro Air Vehicles Maneuvering Based on Bilateral Wings
International Journal of Aerospace Engineering, 2022 With the development and application of a bionic flapping micro aircraft vehicle (FMAV), further requirements for its high maneuvering flight characteristics have been put forward. A controlling tail cannot meet the requirements of the maneuvering flight
Rui Zhang +5 more
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Experimental investigation of some aspects of insect-like flapping flight aerodynamics for application to micro air vehicles [PDF]
, 2009 Insect-like flapping flight offers a power-efficient and highly manoeuvrable basis for micro air vehicles for indoor applications. Some aspects of the aerodynamics associated with the sweeping phase of insect wing kinematics are examined by making ...
Ansari, S. A. +5 more
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Design of Variable Amplitude Flapping Wing Aircraft and Realization of Multiple Flight Modes
Jixie chuandong, 2021 Aiming at the problems of the single flight mode and inflexible flight attitude，a variable amplitude flapping wing aircraft is designed. By adjusting the flapping amplitude， the flapping wing motion attitude and flight mode can be switched.
Yueyang Hou +4 more
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Power Modeling and Experiment Study of Large Flapping-Wing Flying Robot during Forward Flight
Applied Sciences, 2022 A power estimation approach for calculating the power of a flapping-wing air vehicle (FWAV) in forward flight is proposed in this paper. One of the challenges and essential points of FWAVs is endurance.
Siping Zhong, Wenfu Xu
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Journal of Robotics, 2020 The current flapping wing adopts T-shaped or cross-shaped tail fin to adjust its flight posture. However, how the tail fin will affect the hover control is not very clear.
Pingxia Zhang, Junru Zhu, Yongqiang Zhu
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Unsteady aerodynamic characteristics of a bionic flapping wing in three-dimensional composite motion
AIP Advances, 2022 Owing to continual advances in computational fluid dynamics, simulations of fluids have emerged as an important means of analyzing the aerodynamic characteristics of flapping-wing flight.
Lun Li +5 more
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Research progress on the energy consumption of bionic flapping-wing aerial vehicles
工程科学学报, 2022 Natural flyers use muscles, bones, and other structures in coordination to attain agile and nimble flight performance. They can fly in various complex environments through different flight modes, such as flapping, hovering, and gliding.
Min ZHAO +4 more
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Complexity, 2023 Flapping-wing flight control is a multi-input and multi-output nonlinear system with uncertainties, which is affected by modeling errors, parameter variations, external disturbances, and unmodeled dynamics. Parameter uncertainty has a great impact on the
Lun Li +4 more
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