Feasibility of using single three-gimbaled control moment gyro for control of orbital spacecraft modules
Optimization study of a single three-gimbaled control moment gyro Final report
1969-12-01
Report
No indication
English
Nonredundant Single-Gimbaled Control Moment Gyroscopes
Online Contents | 2012
|Nonredundant Single-Gimbaled Control Moment Gyroscopes
AIAA | 2012
|