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
01.12.1969
Report
Keine Angabe
Englisch
Nonredundant Single-Gimbaled Control Moment Gyroscopes
Online Contents | 2012
|Nonredundant Single-Gimbaled Control Moment Gyroscopes
AIAA | 2012
|