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- 津田 雄一
- 宇宙航空研究開発機構宇宙科学研究所
書誌事項
- タイトル別名
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- Spin Stability Criteria for Axisymmetric Spinning Body with Large Flexible Membrane
- ダイ メンセキ ジュウナン マクメン オ ユウスル ジク タイショウ スピン ブッタイ ノ シセイ アンテイ ジョウケン
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抄録
Stability of the dynamics of spinning spacecraft equipped with a large flexible membrane is discussed. The spin stability of an object having a flexible structure is deteriorated from that of a rigid object with the same shape in general, which makes a significant impact on the design of such spacecraft systems. This paper provides a fully analytical solution for the stability criteria of axisymmetric spinner spacecraft equipped with a large flexible membrane. Distinct from past studies, this paper does not impose restrictions on axial offset of the membrane attachment, and provides a stability condition using energy-angular momentum analysis when the membrane is subject only to an outer-plane first-order mode deformation. These criteria can be applied to the design of such missions as spinner solar sail spacecraft, large solar power satellite and other general spacecraft with large axisymmetric structures.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 58 (678), 187-194, 2010
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
- 1390001204470844288
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- NII論文ID
- 10026612808
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 10778824
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
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- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可