テザーシステムを用いた衛星の軌道変更のためのフィードバック制御

外本 伸治, 古賀 笑平

研究成果: Contribution to journalArticle査読

抄録

This study deals with co-planar orbital transfer of a satellite using a tether extension/retrieval mechanism. By controlling the pitch motion of the tether system, the designated velocity increment for the orbital transfer can be achieved at a prescribed position in orbit. First, this paper shows the governing equations of motion of the system by taking into consideration of the tether mass. Then, to achieve the specified tether length, pitch angle, and pitch angular rate at the designated position, this paper proposes two feedback control techniques to reduce the system's state errors: one for the pitch angular momentum error and the other for the pitch angle and pitch angular rate errors. Finally, numerical simulations demonstrate that the proposed methods can successfully achieve the designated states at the specified final position in the orbit.
寄稿の翻訳タイトルFeedback Control for Satellite Orbit Transfer by a Tethered Satellite System
本文言語日本語
ページ(範囲)301-307
ページ数7
ジャーナル日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
57
666
DOI
出版ステータス出版済み - 7 5 2009

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