The Proceedings of the Symposium on the Motion and Vibration Control
Online ISSN : 2424-3000
2011.12
Session ID : A302
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A302 Control of Prop-Hanging Flight of Small Fixed-Wing Airplane Using Angular Velocity Sensor
Yoshitaka MinagawaMitsuo Hirata
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CONFERENCE PROCEEDINGS FREE ACCESS

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Abstract
A prop-hanging is known as a way of flight, and it can achieve hovering without special equipments to change the direction of the thrust. Therefore, it has advantages comparing to the tilt-rotor aircraft or vectored thrust aircraft. However, lots of sensors to measure the position and the attitude of the airplane are required to achieve the prop-hanging by automatic control. Therefore, in this paper, we propose a control method to stabilize the attitude of the airplane by using angular velocity sensors only. The effectiveness of the proposed method is evaluated by simulation and experiment.
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© 2011 The Japan Society of Mechanical Engineers
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