@inproceedings{oai:jaxa.repo.nii.ac.jp:00004430,
 author = {花田, 俊也 and 柳沢, 俊文 and 北澤, 幸人 and Hanada, Toshiya and Yanagisawa, Toshifumi and Kitazawa, Yukihito},
 book = {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, JAXA Special Publication: Proceedings of the 8th Spacecraft Environment Symposium},
 month = {Feb},
 note = {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, 8th Spacecraft Enivironment Symposium (October 18-19, 2011, Tokyo Big Sight), Tokyo Japan, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065159011, レポート番号: JAXA-SP-11-012},
 pages = {63--70},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Research on effective search strategy for unknown space debris},
 volume = {JAXA-SP-11-012},
 year = {2012}
}