This paper presents the results 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.
World Congress of the International Federation of Automatic Control ; 1972 ; Paris, France
01.01.1972
Sonstige
Keine Angabe
Englisch
NTIS | 1972
|NTRS | 1972
|Attitude Control of a Spinning Skylab
AIAA | 1973
|Passive stability of a spinning Skylab
NTRS | 1972
|Attitude control of a spinning Skylab.
NTRS | 1972
|