@inproceedings{oai:jaxa.repo.nii.ac.jp:00005589,
 author = {山田, 克彦 and Yamada, Katsuhiko},
 book = {宇宙航空研究開発機構特別資料: 低推力・連続加速を用いた宇宙ミッションに関する研究会論文集, JAXA Special Publication: Collection of Papers Presented at the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration},
 month = {Feb},
 note = {2機の編隊飛行制御において、従宇宙機が主宇宙機に対して進行方向に一定距離だけ離れた場合を対象に、地球重力のJ(sub 2)項の影響が2機の宇宙機の相対位置にどう影響するかを解析した。その結果に基づき、J(sub 2)項による相対位置変動を低減するための、従宇宙機の初期速度と主宇宙機の軌道離心率の設定について考察した。また相対位置変動を除去するために、従宇宙機に連続的に入力を加える場合の連続入力の大きさを求め、主宇宙機の軌道離心率を適切に設定することで連続入力の変動をある程度抑えられることを述べた。, In this paper, precise position keeping of a deputy spacecraft with respect to a chief spacecraft is considered in the formation flight. Especially, the case where the deputy spacecraft is located at the certain distance from the chief spacecraft in the tangential direction is analyzed under the J(sub 2) perturbation. The relative position between the two spacecraft is affected by the J(sub 2) perturbation, and the two methods to compensate the J(sub 2) effects are considered. One is to set the initial velocity of the deputy spacecraft and the eccentricity of the chief spacecraft orbit to alleviate the relative position variation. The other one is to add the low thrust force to the deputy spacecraft to cancel the J(sub 2) effects. These two cases are analyzed and the appropriate control values are derived to compensate the J(sub 2) perturbation., 資料番号: AA0063739007, レポート番号: JAXA-SP-07-020},
 pages = {39--48},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {低推力を用いた編隊飛行制御の解析},
 volume = {JAXA-SP-07-020},
 year = {2008}
}