NASA NTRS · 19720006151
Drag-free satellite control system technology
Abstract
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.
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Debra, D. B.. 1971-11-01. Drag-free satellite control system technology. https://ntrs.nasa.gov/citations/19720006151
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