Modeling of Solar Radiation Pressure Effect for Trajectory Guidance of Spinner Solar Sailer IKAROS
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- TSUDA Yuichi
- Japan Aerospace Exploration Agency
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- SAIKI Takanao
- Japan Aerospace Exploration Agency
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- FUNASE Ryu
- Japan Aerospace Exploration Agency
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- MIMASU Yuya
- Japan Aerospace Exploration Agency
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- YAMAGUCHI Tomohiro
- Japan Aerospace Exploration Agency
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- IKEDA Hitoshi
- Japan Aerospace Exploration Agency
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- NAKAMIYA Masaki
- Japan Aerospace Exploration Agency
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- TAKEUCHI Hiroshi
- Japan Aerospace Exploration Agency
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- IKAROS Demonstration Team
- Japan Aerospace Exploration Agency
抄録
This paper describes a modeling of attitude dynamics of spinning solar sail spacecraft under influence of solar radiation pressure (SRP). This method is verified and actually exploited in the attitude and trajectory guidance operation of Japanese interplanetary solar sail demonstration spacecraft IKAROS. IKAROS shows a unique attitude behavior due to strong SRP effect. This paper introduces a new generalized dynamics model called Generalized Spinning Sail Model (GSSM), which clearly explains physics behind the observed phenomena with only three parameters. Precise understanding of attitude dynamics through the GSSM led to 6 months of world first interplanetary trajectory guidance of solar sail-craft toward Venus. The GSSM also contributed to realize a zero-fuel spin axis maintenance for most of the flight path before the Venus flyby. In this paper, an overview of IKAROS attitude and trajectory control operation in the cruising phase, derivation of the proposed model and its implementation to the actual IKAROS operation are shown.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 10 (ists28), Po_4_7-Po_4_12, 2012
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
- 1390282680297061888
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- NII論文ID
- 130002136546
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- ISSN
- 18840485
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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
- CiNii Articles
- KAKEN
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- 抄録ライセンスフラグ
- 使用不可