@article{oai:jaxa.repo.nii.ac.jp:00022425,
 author = {Torisaka, Ayako and 小澤, 悟 and Yamakawa, Hiroshi and Kobayashi, Nobuyuki and Torisaka, Ayako and Ozawa, Satoru and Yamakawa, Hiroshi and Kobayashi, Nobuyuki},
 issue = {1},
 journal = {Journal of Space Engineering},
 month = {Dec},
 note = {This paper proposes a relative position and attitude control method by using onlymagnetic force with multi-dipole for formation-flying spacecrafts. The controlmethod can be widely applied to re-configurable space structures that architect largestructure or reconstruct themselves by assembling basic structural units. Oneremarkable benefit of the method is that it does not require reaction wheels forrelative attitude controls and then doesn't require any fuel for unloading. This paperfocuses on current control of dipoles which produce strong nonlinear magneticforces and suggests a way of linearization by using a corresponding linear referencesystem. A feasibility of this method and controllability of the strong nonlinearsystem is discussed, and then the series of position and attitude control simulationare shown, and the future works are suggested in the paper., 資料番号: PA1410061000},
 pages = {44--55},
 title = {Control of Electromagnetic Current at Final Docking Phase of Small Satellites},
 volume = {6},
 year = {2013}
}