当前位置：
X-MOL 学术
›
Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.
›
论文详情
Our official English website, www.x-mol.net, welcomes your
feedback! (Note: you will need to create a separate account there.)
Attitude control of nanosatellite with single thruster using relative displacements of movable unit
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-09-20 , DOI: 10.1177/0954410020959868 Anton V Doroshin 1 , Alexander V Eremenko 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-09-20 , DOI: 10.1177/0954410020959868 Anton V Doroshin 1 , Alexander V Eremenko 1
Affiliation
The attitude dynamics of a nanosatellite (NS) with one movable unit changing its angular position relative to a main body of the nanosatellite is considered. This relative movability of the unit ca...
中文翻译：
基于可动单元相对位移的单推进器纳米卫星姿态控制
考虑了具有一个可移动单元的纳米卫星 (NS) 的姿态动力学，该单元改变其相对于纳米卫星主体的角位置。单位的这种相对可移动性...
更新日期：2020-09-20
中文翻译：
基于可动单元相对位移的单推进器纳米卫星姿态控制
考虑了具有一个可移动单元的纳米卫星 (NS) 的姿态动力学，该单元改变其相对于纳米卫星主体的角位置。单位的这种相对可移动性...
京公网安备 11010802027423号