Feasible angular momentum of spacecraft installed with control moment gyros

@inproceedings{Leeghim2018FeasibleAM,
  title={Feasible angular momentum of spacecraft installed with control moment gyros},
  author={Henzeh Leeghim and Jaehyun Jin and Sung-Hoon Mok},
  year={2018}
}
Abstract In this paper, a fundamental approach to analyzing the maneuverability of spacecraft with mounted control moment gyros is addressed by searching feasible angular momentum. The geometrical array of control moment gyros considered is a roof array also known as a 2-SPEED system. Due to the simplicity of the singularity envelope of the array considered, it is reasonably practical to conduct rotational performance analysis of the spacecraft. This maneuverability analysis technique uses a… CONTINUE READING