@inproceedings{oai:jaxa.repo.nii.ac.jp:00007662,
 author = {堀家, 尚子 and 斎藤, 徹 and 前田, 健 and 橋本, 樹明 and Horike, Naoko and Saito, Tetsu and Maeda, Ken and Hashimoto, Tatsuaki},
 book = {平成16年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers},
 month = {Mar},
 note = {一般に、衛星慣性モーメント(MOI)は地上での開発試験フェーズで測定される。しかし、ASTRO-E2衛星のように、衛星に大量の冷媒を搭載している場合などにおいては、軌道上でMOIを測定する必要性がでてくる。本稿では、衛星の保有する角運動量の保存則を基本とし、軌道上の姿勢マヌーバ時に得られるテレメトリデータを用いてMOIを推定する。, Usually, the satellite moment of inertia (MOI) is measured in the satellite system test on the ground. However, it is sometimes required to be estimated in flight condition. For example, ASTRO-E2 satellite has large amount of coolant for the X-ray detector and the coolant evaporates gradually, which causes the change of MOI. In this paper, an estimation scheme of a satellite MOI in-flight is introduced. The estimation scheme uses the satellite telemetry data during attitude maneuver and it is based on the conservation law of a satellite angular momentum., 資料番号: AA0047897029},
 pages = {164--169},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {In-flight estimation method of a satellite moment of inertia},
 year = {2005}
}