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宇宙飛しょう体の直接式最適誘導法
https://jaxa.repo.nii.ac.jp/records/44403
https://jaxa.repo.nii.ac.jp/records/4440380b1c16c-4c11-467b-ba78-eeef7260b4e7
名前 / ファイル | ライセンス | アクション |
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naltr00161.pdf (1.0 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 宇宙飛しょう体の直接式最適誘導法 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | An Optimal Explicit Guidance Equation for Space Vehicle | |||||
著者 |
新田, 慶治
× 新田, 慶治× 松島, 弘一× 大坪, 孔治× 志甫, 徹× NITTA, Keiji× MATSUSHIMA, Koichi× OTSUBO, Kohji× SHIHO, Toru |
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著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所計測部 | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Instrumentation and Control Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-161 巻 161, p. 11, 発行日 1968-08 |
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ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0161000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-161 |