Old Web
English
Sign In
Acemap
>
Paper
>
Concept Design and Development of 30kg Microsatellite HIBARI for Demonstration of Variable Shape Attitude Control
Concept Design and Development of 30kg Microsatellite HIBARI for Demonstration of Variable Shape Attitude Control
2019
Kei Watanabe
Yuhei Kikuya
Yusuke Shintani
Kenichi Sasaki
Hiroki Ando
Tsuyoshi Nakashima
Kiyona Miyamoto
Kaoru Matsubara
Keywords:
Microsatellite
Attitude control
Control theory
Computer science
Correction
Source
Cite
Save
Machine Reading By IdeaReader
0
References
0
Citations
NaN
KQI
[]