Zobrazeno 1 - 10
of 23
pro vyhledávání: '"MURANAKA, Noboru"'
Autor:
Demura, Hirohide, Kobayashi, Shingo, Nemoto, Etsuko, Matsumoto, Naoya, Furuya, Motohiro, Yukishita, Akira, Muranaka, Noboru, Morita, Hideo, Shirakawa, Ken, Maruya, Makoto, Ohyama, Hiroshi, Uo, Masashi, Kubota, Takashi, Hashimoto, Tatsuaki, Kawaguchi, Jun'ichiro, Fujiwara, Akira, Saito, Jun, Sasaki, Sho, Miyamoto, Hideaki, Hirata, Naru
Publikováno v:
Science, 2006 Jun 01. 312(5778), 1347-1349.
Externí odkaz:
https://www.jstor.org/stable/3846369
Autor:
Muranaka, Noboru, Maruya, Makoto, Oyama, Hiroshi, Uo, Masashi, Morita, Hideo, Kubota, Takashi, Hashimoto, Tatsuaki, Saito, Jun, Kawaguchi, Junichiro
Publikováno v:
第16回アストロダイナミクスシンポジウム講演後刷り集 2006 = Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics. :157-166
2005年9月30日〜10月26日に亘って小惑星Itokawaから1〜11kmの距離で取得された139枚の画像を用いて、小惑星に相対的な画像取得位置とカメラ姿勢を推定した。スタートラッカで決定される慣
Autor:
NINOMIYA, Keiken, HASHIMOTO, Tatsuaki, IIDA, Hiroshi, Uo, Masashi, MURANAKA, Noboru, MAEDA, Ken, OGURA, Naoto, SAITOH, Tetsu, FUJIWARA, Koetsu
Publikováno v:
宇宙科学研究所報告. 102:1-88
本報告書は, 宇宙科学研究所のこれまでおよび近い将来の天文観測用科学衛星の姿勢決定系に採用されてきたカルマンフィルタに関して, そのアルゴリズムおよび実用上の工夫を中心に記
Autor:
NINOMIYA, Keiken, OGAWARA, Yoshiaki, HASHIMOTO, Tatsuaki, HIROKAWA, Eiji, MURANAKA, Noboru, MAEDA, Ken, FUJIWARA, Kouetsu, IIDA, Hiroshi, KAWAHARA, Tetsuo, KIMURA, Masabumi, TAKAYASU, Hoshiko
Publikováno v:
宇宙科学研究所報告. 81:1-92
本報告では, 1991年8月30日に M-3S II-6 号ロケットにより打ち上げられた"ようこう"の姿勢制御系に関する詳細な説明を行う。"ようこう"は近地点高度約500km, 遠地点高度約800km, 軌道傾斜角約31
Autor:
TAKAHASHI, Keiji, KOHBATA, Masahiko, USHIROKAWA, Akio, ORII, Takeshi, TOMITA, Hideo, MURANAKA, Noboru, HARA, Hironori
Publikováno v:
東京大学宇宙航空研究所報告. 16(1_B):125-147
資料番号: SA0125822000
Autor:
Ogawara, Yoshiaki, Matsuoka, Masaru, Miyamoto, Shigenori, Muranaka, Noboru, Nishimura, Jun, Oda, Minoru
Publikováno v:
ISAS Research Note. 5:1-12
Note: Presented at the Symposium on Fast Transients in X- and Gamma-rays (May 29-31, 1975, Varna, Bulgaria)
資料番号: SA8000885000
資料番号: SA8000885000
Autor:
HINADA, Motoki, NAKATANI, Ichiro, NINOMIYA, Keiken, MURANAKA, Noboru, NAMERA, Takakazu, UO, Masahi, OGURA, Naoto
Publikováno v:
The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1987. 6:137-147
Analysis is given for the dynamics of a spinning satellite with four radial wire antennas. In this analysis, generalized model is used, in which, mass properties of wire antennas are not equal and antennas' attachment points on the satellite have som
Autor:
NINOMIYA, Keiken, UESUGI, Kuninori, KAWAGUCHI, Junichiro, YOKOTA, Hiroki, MURANAKA, Noboru, NAMERA, Takakazu, KITADE, Kenji, OGASAWARA, Masahiro, KIMURA, Masahumi, DOBASHI, Masayuki
Publikováno v:
宇宙科学研究所報告. 33:1-45
To support the operation of onboard AOCS (Attitude and Orbit Control System) of "SAKIGAKE" and "SUISEI", ground support software for attitude control and orbit correction was developed. The software, named POPS (PLANET-A AOCS Operation Software), has
Publikováno v:
ISAS Research Note. 4:1-30
Note: Invited Paper at the Symposium on the Techniques of Solar and Cosmic X-ray Spectroscopy (May 22-23, 1975, London)
資料番号: SA8000886000
資料番号: SA8000886000
Publikováno v:
ISAS Research Note. 29:1-24
資料番号: SA8000861000