Kyushu University
Japan Aerospace Exploration Agency (JAXA)
IHI
出版者
宇宙航空研究開発機構
出版者(英)
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料: 第8回宇宙環境シンポジウム講演論文集
雑誌名(英)
JAXA Special Publication: Proceedings of the 8th Spacecraft Environment Symposium
巻
JAXA-SP-11-012
ページ
63 - 70
発行年
2012-02-20
会議概要(会議名, 開催地, 会期, 主催者等)
第8回宇宙環境シンポジウム (2011年10月18-19日. 東京国際展示場), 東京
会議概要(会議名, 開催地, 会期, 主催者等)(英)
8th Spacecraft Enivironment Symposium (October 18-19, 2011, Tokyo Big Sight), Tokyo Japan
抄録(英)
This paper proposes to apply the orbital debris modeling techniques to devise an effective search strategy applicable for breakup fragments in the geostationary region. The orbital debris modeling techniques describe debris generation and propagation to effectively conduct predictive analyses of space objects that include characterizing, tracking and predicting the behavior of individual and groups of space objects. Therefore, the techniques enable us to predict population of debris from a specific breakup. The population prediction specifies effectively when, where and how we should conduct optical measurements using ground-based telescopes. The orbital debris modeling techniques also enable us to predict motion of debris in successive images. The motion prediction specifies effectively and precisely how we should process successive images of objects in the geostationary region, taken with ground-based telescopes. This paper also validates the proposed search strategy through actual observations, targeting the US Titan IIIC transtage explosion in the geostationary region.
内容記述
形態: カラー図版あり
内容記述(英)
Physical characteristics: Original contains color illustrations