Development of Bird-like Micro Aerial Vehicle with Flapping and Feathering Wing Motions

スポンサーリンク

概要

• 論文の詳細を見る

• To investigate the feasibility of a highly efficient flapping system capable of avian maneuvers, such as rapid takeoff, hover and gliding, a full scale bird-like (ornithopter) flapping-wing micro aerial vehicle (MAV) shaped and patterned after a typical pigeon (Columba livia) has been designed and constructed. Both numerical and experimental methods have been used in the development of this vehicle. This flapping-wing micro aerial vehicle utilizes both the flapping and feathering motions of an avian wing by employing a novel flapping-feathering mechanism, which has been synthesized and constructed so as to best describe the properly coordinated flapping and feathering wing motions at phase angle difference of 90° in a horizontal steady level flight condition. This design allows high flapping and feathering amplitudes and is configurable for asymmetric wing motions which are desirable in high-speed flapping flight and maneuvering. The preliminary results indicate its viability as a practical and an efficient flapping-wing micro aerial vehicle.

• 2008-05-04

著者

• MAGLASANG Jonathan

  Department of Aeronautics and Astronautics, Kyushu University

• GOTO Norihiro

  Department of Aeronautics and Astronautics, Kyushu University

• ISOGAI Koji

  Department of Aerospace Engineering, Nippon Bunri University

• Isogai Koji

  Department Of Aerospace Engineering Nippon Bunri University

• Maglasang Jonathan

  Department Of Aeronautics And Astronautics Kyushu University

• Goto Norihiro

  Department Of Aeronautical Engineering Faculty Of Engineering Kyushu University

• Isogai Koji

  Department Of Aerospace Engineering Nihonbunri University

関連論文

• Development of Bird-like Micro Aerial Vehicle with Flapping and Feathering Wing Motions
• Transition Flight Simulation of Flapping-Wing Micro-Aerial Vehicle Using Aerodynamic Database
• Optimum Aeroelastic Design of Resonance Type Flapping Wing for Micro Air Vehicle
• Resonance Type Flapping Wing for Micro Air Vehicle
• Aerodynamic Study and Mechanization Concepts for Flapping-Wing Micro Aerial Vehicles
• Implementation of Robust Stability Augmentation Systems for a Blimp
• Shape Optimization of Fish Tail Propulsion with Hydro-Elastic Effects
• Nonlinear Dynamical Analysis for a Reentry Vehicle
• Identification of Blimp Dynamics via Flight Tests
• A New Approach to Airborne Mine Detection Scheme Using a Magnetic Gradiometer
• On the Root Locus Method Applied to Flexural Vibration Control Systems
• Analysis, Evaluation and Display Design for Pilot-Vehicle Systems via Modern Optimal Control Approach
• Optical Bistability of Terthiophene/Poly(methyl methacrylate) Composite Film Prepared Using Spin-Coating
• Catalytic hydrogenolysis of 1,1-dichloro-3-methyl-2-phenylcyclopropane.
• Catalytic hydrogenolysis of 1,1-difluoro-2-phenyl- and 1,1-difluoro-3-methyl-2-phenylcyclopropane.

もっと見る 閉じる

スポンサーリンク