Tether Actuator to Control Vibration of Space Structures
- Paper number
IAC-14,D1,2,5,x24927
- Author
Prof. Hironori FUJII, Kanagawa Institute of Technology, Japan
- Coauthor
Prof. Takeo WATANABE, Teikyo University, Japan
- Coauthor
Prof. Tairou Kusagaya, Tokyo Metropolitan College of Industrial Technology, Japan
- Coauthor
Mr. Kenichi Anma, Mitsubishi Heavy Industries, Ltd., Japan
- Coauthor
Prof. Jixiang Fan, Harbin Normal University, China
- Year
2014
- Abstract
A Space Solar Power Satellite (SSPS) proposed by a Japanese organization is an example to employ tether technology to enhance the attitude stability of the system passively. The system consists of large flexible solar panel connected to a bus system through four tethers, and the gravity-gradient torque is utilized to stabilize its attitude with employment of the tether technology. This paper is devoted to study a control method of the vibration of the large flexible solar panel using tether as actuators. The tether tension is employed to control the vibration of the solar panel. Effectiveness is examined experimentally in this paper for vibration suppression on the tethered flexible space structures (SSPS) by employing a micro tension actuator. In the experiment, a micro tension actuator is used to generate very small tension and control the structure vibration. The micro tension actuator employs with a very flexible arm connected to tether in order to overcome the penalty of nonlinear behavior of tether. The control performance of the micro tension actuator is examined in its performance to suppress flexible structure connected through tether. Time responses of the vibration is shown. It is seen that the vibration of the panel is well controlled although tether is ysed to only pull but not push. The experiment results have verified the validity of this controller and the ability is confirmed on the vibration suppression of the micro tension actuator.
- Abstract document
- Manuscript document
IAC-14,D1,2,5,x24927.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.