Damping Control by One-Axis Magnetic Torquer and Gravity Gradient Attitude Stabilization for Small Satellite

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概要

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• A Whale Ecology Observation Satellite (WEOS) was successfully launched on December 14th, 2002. We adopted a single-axis magnetic torquer damping control and gravity gradient attitude stabilization for WEOS. It is the first trial in Japan for pointing communications antennas towards Earth, and the GPS antenna towards zenith. The damping control and attitude stabilization system of WEOS consists of a three-axis magnetometer, a magnetic torquer coil, a deployable mast with a fixed mass at the tip, and attitude control software. This system carried out rate damping control of the principal axis of the maximum moment of inertia and earth pointing attitude stabilization. Immediately after separation from the H-IIA-4 launch vehicle, WEOS tumbled due to the imbalance force of the three separation springs. The tumbling was reduced by the closed-loop damping control and then the mast was deployed. After 1 week, we confirmed the establishment of the gravity gradient attitude stabilization. This paper describes the attitude control system, operation procedure, and control results.

• 2006-08-04

著者

• Hosokawa Shigeru

  General Research Institute Chiba Institute Of Technology

• Masumoto Yoshinari

  Deu Aerospace Consulting Office

• TAKEZAWA Susumu

  Wel Research, Co. Inc.

• HANEJI Kazuhiko

  Wel Research, Co. Inc.

• Takezawa Susumu

  Wel Research Co. Inc.

• Haneji Kazuhiko

  Wel Research Co. Inc.

関連論文

• Development of a 10 Kg-class Micro Satellite for the Observation of Sprites and Atmospheric Lightning Events(WSANE2006)
• Whale Ecology Observation Satellite System And Its Applications(Small satellite (2), Workshop for Space, Aeronautical and Navigational Electronics (W S A N E 2005))
• Damping Control by One-Axis Magnetic Torquer and Gravity Gradient Attitude Stabilization for Small Satellite

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