In order to improve the flight performance of the flapping-wing aircraft,a novel multi-degree of freedom flapping-wing mechanism based on the space pendulum mechanism was designed by referring to the flight motion characteristics of living things.
FANG Yue, YANG Ye
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Development of a novel flapping wing micro aerial vehicle with elliptical wingtip trajectory [PDF]
This paper describes a novel flapping wing micro air vehicle (FWMAV),which can achieve two active degree of freedom (DOF) movements of flapping and swing, as well as twisting passively.
Q. Liu +6 more
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Design and Analysis of A Two-stage Bionic Flapping Wing Aircraft
Abstract To develop an aircraft with a certain load capacity, high lift, and high bionics, a two-stage bionic flapping wing aircraft was designed according to the physiological structure of large birds. Firstly, the degrees of freedom of the transmission mechanism of flapping wing aircraft are calculated, and the dimensions of each ...
Xiaokun Fu +3 more
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Novel Dihedral-Based Control of Flapping-Wing Aircraft With Application to Perching [PDF]
We describe the design of an aerial robot inspired by birds and the underlying theoretical developments leading to novel control and closed-loop guidance algorithms for a perching maneuver. A unique feature of this robot is that it uses wing articulation to control the flight path angle as well as the heading angle.
Aditya A. Paranjape +2 more
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Effects of airfoil on aerodynamic performance of flapping wing
Flapping-wing aircraft (FWA) operates in a flight mode that mimics natural flyers, such as birds, bats and insects. For large scale bird-inspired flapping wings aircraft, the design of airfoil parameters is crucial to improving the aerodynamic ...
Min Zhao, Yao Zou, Qiang Fu, Wei He
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Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft
Aiming at the problems of single flapping wing movement mode and low flight flexibility and stability of flapping-wing aircraft, a single-drive multi-mode flapping-wing aircraft based on the space linkage mechanism is designed. The kinematic model of the
Jiang Houqing, Hou Yu, Guo Yongxing
doaj
Design of Variable Amplitude Flapping Wing Aircraft and Realization of Multiple Flight Modes
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
doaj
Investigation of the Influence of Different Flapping Wing Motion Characteristics on Aerodynamic Parameters under Incoming Flow [PDF]
There is high flight efficiency of flapping wing aircraft, and its hovering ability, wind loading rating, maneuverability and concealment are better than that of multi-rotor and fixed-wing aircraft. In this paper, the bionic flapping wing is taken as the
Z. Guo +4 more
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Design and Aerodynamic Analysis of Flapping Mechanism of Two-stage Flapping-wing Aircrafts
In order to improve the flight performance of the flapping-wing aircraft, this study draws on the characteristics of the flight movement of large birds, designs a new two-stage foldable bionic flapping-wing mechanism, and establishes the kinematic and ...
Sheng Dian +3 more
doaj
Dynamic Analysis of the Flapping Mechanism of Flapping Wing Aircraft
Abstract In order to improve the design level of bionic flapping-wing aircraft, it is necessary to find out the influence of load undulating moment on the motor under the action of air undulating moment. This paper takes flapping-wing aircraft with a crank and rocker mechanism as a flapping mechanism as an example.
Wei He +4 more
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