Navigation of Small and Lightweight Helicopter

スポンサーリンク

概要

• 論文の詳細を見る

• A small battery-powered helicopter with a total weight of about 200 g and a rotor diameter of about 35 cm has been developed. Some indoor flights were performed without a human operator using a transmitter. The helicopter is capable of autonomous hovering flight near walls when IR range finders mounted on it are used to measure distances to walls and the floor. Four mounted photodetectors permit two maneuvers. In the first maneuver, the helicopter can follow a moving light. So it can be controlled simply by moving a light, and can follow a robot or a person carrying a light. In the second maneuver, the helicopter flying over a first light can fly towards a second light, when the first light is turned off and the second light is turned on. The position of the helicopter can be controlled by successively switching (on and off) lights in a row.

• 社団法人 日本航空宇宙学会の論文
• 2005-11-04

著者

• TOKUTAKE Hiroshi

  Faculty of Mechanical Engineering, Kanazawa University

• Sunada Shigeru

  Department Of Aerospace Engineering Osaka Prefecture University

• SUNADA Shigeru

  Osaka Prefecture University

• TOKUTAKE Hiroshi

  Osaka Prefecture University

• Sunada Shigeru

  National Institute Of Advanced Industrial Science And Technology:(present Address) Department Of Aer

• MATSUE Atsushi

  Department of Aerospace Engineering, Osaka Prefecture University

• MATSUE Atsushi

  Osaka Prefecture University

• HIROSUE Wataru

  Osaka Prefecture University

• OHKURA Akihiro

  Osaka Prefecture University

• Tokutake Hiroshi

  Faculty Of Mechanical Engineering Kanazawa University

関連論文

• Attitude Control of a Small UAV Using a Flow Sensor System
• Optical Measurement of the Deformation, Motion, and Generated Force of the Wings of a Moth, Mythimna Separata : Walker
• Fluid Dynamic Forces Acting on Rectangular Plate with Hole in Stokes Flow
• Active Control of Flapping Wings Using Wing Deformation
• Disturbance Observer Based on Multipoint Feedback
• Fluid Dynamic Forces Acting on Rectangular Plate with Hole in Stokes Flow
• Characteristics of Rotary Wings in Hovering Mode at an Ultra-Low Reynolds Number
• Analysis of Bell-Hiller Stabilizer Bar
• Analysis of Flapping Motion of Rotors of Small Coaxial Helicopter
• Navigation of Small and Lightweight Helicopter
• Disturbance Observer Based on Multipoint Feedback
• Flight Stability of an Airplane on Mars
• Disturbance Preview Controller and Its Application to a Small UAV
• A Split-wing Micro Air Vehicle
• A Split-wing Micro Air Vehicle

もっと見る 閉じる

スポンサーリンク