AUTONOMOUS FLIGHT CONTROL OF RADIO-CONTROLLED HELICOPTER SKY SURVEYOR

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概要

• 論文の詳細を見る

• This paper describes the stabilizing control system design for small-scale helicopter based unmanned aerial vehicle Sky Surveyor. For full-autonomous control, the original hardware and software which can be equipped with small-scale helicopter, including small-sized lightweight control unit, have been newly developed. System identification method has been used for analysis of system dynamics in the frequency domain and the time domain. On-axis input/output data collected through the identification flight experiment achieved a coherence close to unity, and reliable transfer functions could been calculated. The modern control theory was applied to design lumped control system which can stabilize velocities of a fuselage. Good control performance has been shown in simulation.

• 一般社団法人日本機械学会の論文

著者

• SHIN Jinok

  Chiba University

• FUJIWARA Daigo

  Chiba University

• HAZAWA Kensaku

  Chiba University

• NONAMI Kenzo

  Faculty of Engineering, Chiba University

• Fujiwara Daigo

  Graduate School of Science and Technology, Chiba University

• Shin Jinok

  Graduate School of Science and Technology, Chiba University

• Hazawa Kensaku

  Graduate School of Science and Technology, Chiba University

• Nonami Kenzo

  Faculty Of Engineering Chiba University

関連論文

• 121 Model-based Attitude and Hovering Control of Small Unmanned Helicopter
• Sliding Mode Servo Controller Design for Sensorless Flexible Rotor-Magnetic Bearing Systems with VSS Disturbance Observer
• AUTONOMOUS FLIGHT CONTROL OF RADIO-CONTROLLED HELICOPTER SKY SURVEYOR
• A DESIGN METHOD FOR SLIDING MODE CONTROL WITH BACKSTEPPINTG HYPERPLANE
• A209 Localization of MAV in GPS-Denied Environment Using Embedded Stereo Camera

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