@article{oai:jaxa.repo.nii.ac.jp:00022672,
 author = {大野, 剛 and 津田, 雄一 and 赤塚, 康祐 and 佐伯, 孝尚 and 三桝, 裕也 and 尾川, 順子 and 照井, 冬人 and Ono, Go and Tsuda, Yuichi and Akatsuka, Kosuke and Saiki, Takanao and Mimasu, Yuya and Ogawa, Naoko and Terui, Fuyuto},
 issue = {7},
 journal = {Journal of Guidance, Control, and Dynamics},
 month = {May},
 note = {This paper describes a method of modeling general attitude dynamics of a nonspinning momentum-biased spacecraft under strong influence of solar radiation pressure. This model, called the “generalized sail dynamics model,” can be applied to realistic solar sail spacecraft with nonflat surfaces and nonuniform optical reflectance. A coarse sun-pointing momentum-biased spacecraft is especially of interest, for which an approximate solution of the equations of motion is analytically derived. Stability and fundamental characteristics of momentum-biased spacecraft dynamics as well as theoretical relations with past dynamics models are discussed in detail. Furthermore, unique attitude motion predicted by the novel model is verified with flight data of the Japanese interplanetary probe, Hayabusa 2., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: PA1610053000},
 pages = {1491--1500},
 title = {Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft},
 volume = {39},
 year = {2016}
}