Transition Flight Simulation of Flapping-Wing Micro-Aerial Vehicle Using Aerodynamic Database

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概要

• 論文の詳細を見る

• The paper describes how to simulate the flight of a flapping-wing micro-aerial vehicle (MAV). It uses an aerodynamic database generated using three-dimensional Navier-Stokes code. The database is composed of the time mean aerodynamic forces and moments generated at various flapping wing motions in various flight modes. Flight is simulated utilizing the database by interpolation. The procedure is applied to transition flight of a dragonfly-type MAV with two-pairs of resonance-type flapping wings. The present MAV attains the mission of hovering, transition and cruising flights successfully with stable attitude.

• 2010-08-04

著者

• ISOGAI Koji

  Department of Aerospace Engineering, Nippon Bunri University

• Isogai Koji

  Department Of Aerospace Engineering Nippon Bunri University

• KAWABE Hiroyasu

  Department of Aerospace Engineering, Nippon Bunri University

• Kawabe Hiroyasu

  Department Of Aerospace Engineering Nippon Bunri University

• Isogai Koji

  Department Of Aerospace Engineering Nihonbunri University

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