The results of an analytical investigation of the rotational dynamics of a spinning Skylab space station are presented. The passive stability of motion of a simplified model consisting of a rigid core body with two attached flexible appendages is investigated. The parameter plane stability technique is applied to the specific Skylab case to determine its transient response to external disturbances. (Author)
Passive Stability of a Spinning Skylab
1972
22 pages
Report
Keine Angabe
Englisch
Passive stability of a spinning Skylab
NTRS | 1972
|Passive Stability of a Spinning Skylab
AIAA | 1972
|NTIS | 1972
|Stabilizing a spinning Skylab.
NTRS | 1972
|NTRS | 1972
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