Development of Flapping Robot with Self-Takeoff from The Ground Capability

Afakh, Muhammad Labiyb; Sato, Terukazu; SATO, Hidaka; Takesue, Naoyuki

doi:10.1109/icra48506.2021.9561656

Cited by 8 publications

(3 citation statements)

References 15 publications

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“…omega [2] indicates that the wing flutter axis is the z-axis. In order to conveniently constrain the degree of freedom of a rigid body in a particular direction.…”

Section: Pneumatic Calculation Programmementioning

confidence: 99%

“…In the 1950s, Anderson and Richards observed that the structure of a butterfly's wing has many tiny tile-like structural scales, a structure that allows the wing to remain relatively lightweight while maintaining sufficient strength [1] . The bionic flapping wing robot developed by the Tokyo Metropolitan University research team can use a simple flapping mechanism and lightweight design to generate thrust by exceeding its own weight [2] . Xu Yixing of Harbin Institute of Technology has designed and built a prototype of a bionic bat flapping wing aircraft.…”

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Numerical simulation of aerodynamic characteristics of butterfly-like flapping wing aircraft based on Ansys Fluent

Qian,

Li,

Guo

et al. 2024

Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024)

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“…omega [2] indicates that the wing flutter axis is the z-axis. In order to conveniently constrain the degree of freedom of a rigid body in a particular direction.…”

Section: Pneumatic Calculation Programmementioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

Numerical simulation of aerodynamic characteristics of butterfly-like flapping wing aircraft based on Ansys Fluent

Qian,

Li,

Guo

et al. 2024

Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024)

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“…In this mechanism, the pitching moment has a huge effect on the performance of the ornithopter, especially at initial take-off. Future research must be focused on developing self-take-off capabilities such as in OrnibiBot [9]. Limited research is done on medium-sized ornithopters.…”

Section: Literature Reviewmentioning

confidence: 99%

Conceptual Study of Ornithopter for Better Future Performance and Application

Akash,

Mansoori,

Mazumder

et al. 2023

Advances in Science and Technology

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An ornithopter is a power-driven aircraft that utilizes a flapping mechanism. This paper summarized the research and development carried on Unmanned Aerial Vehicle (UAV) till date and reclaims the efficiency on ornithopter namely the flapping frequency, Reynold number, kinematics, transmission system and flapping mechanisms. The present investigation explores the design of a biologically inspired flying Unmanned Aerial Vehicle. For its execution, varied of analyses of flight mechanics, stability, and the control of flapping motion. The theoretical techniques involved in the construction of an ornithopter have investigation for surveillance, military application, spy work, and rescue operations. Additionally, the material used for construction of ornithopter is also discussed. The benefits of the flapping mechanism for are not limited. This paper also reviews the research and development done on the previous UAVs and from small birds to large birds. In this paper the experimental analysis has been done on the ANSYS Fluent on a semi elliptical wing design with a wingspan of 0.25m which delivered the output of how the wind flow and pressure can affect the efficiency of a flapping wing according to the varying angle of attack. This concluded the selection of a material with low stiffness.

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