Experimental Verification for Attitude Control of Spacecraft Utilizing Double-Gimbal Variable-Speed Control Moment Gyroscopes
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- KANATA Sayaka
- Department of Aerospace Engineering, Osaka Metropolitan University
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- HAYASHIDA Futa
- Department of Aerospace Engineering, Osaka Prefecture University
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- SHIMOMURA Takashi
- Department of Aerospace Engineering, Osaka Metropolitan University
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説明
<p>Double-gimbal variable-speed control momentum gyroscopes (DGVSCMGs) have been attracting attention as actuators for satellite attitude control. The DGVSCMG has the advantage in that it can provide three-axis torque using a single unit, and various control methods have been actively investigated. However, previous studies only evaluated control performance via numerical simulations. The authors experimentally evaluate the control performance of the proposed DGVSCMG for practical verification. An experimental DGVSCMG machine was fabricated and three-axis attitude control in the gravity environment of an indoor experiment was achieved. The results are compared with numerical simulation results to confirm the validity of the proposed dynamics model and control system.</p>
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 66 (6), 209-216, 2023
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390016572035854464
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- ISSN
- 21894205
- 05493811
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- Crossref
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- 抄録ライセンスフラグ
- 使用不可