The results are presented of a study of the dynamics of a spinning Skylab space station. The stability of motion of several simplified models with flexible appendages was investigated. A digital simulation model that more accurately portrays the complex Skylab vehicle is described, and simulation results are compared with analytically derived results.
Stabilizing a spinning Skylab
1972-01-03
Report
No indication
English
NTIS | 1972
|Stabilizing a spinning Skylab.
NTRS | 1972
|Attitude Control of a Spinning Skylab
AIAA | 1973
|Attitude control of a spinning Skylab.
NTRS | 1972
|Attitude control of a spinning Skylab
AIAA | 1972
|