Some of the technology developed in building a drag-free satellite simulator for laboratory use is described. The design decisions made in order to achieve a 10 to the -11th power g perturbation level for the navigation satellite is discussed. The control system development that will make possible drag-free operation of spinning satellites to reduce perturbation levels by averaging is described.
Drag-free satellite control system technology
1971-11-01
Miscellaneous
No indication
English
NTRS | 1989
|Drag-free satellite control : final report
TIBKAT | 1998
|AIAA | 1964
|Integral control of a spinning drag-free satellite
AIAA | 1977
|High stability control of earth observation satellite based on drag-free technology
Tema Archive | 2009
|