The design and testing of an experimental pressure regulator satellite attitude control using electronic feedback are described. It is shown that, using readily available components, the regulator can maintain a controlled pressure from zero up to supply pressure to within an accuracy of a few per cent. The limitations of the experimental controller were shown to be due to the type of value and drive circuit used. (Author)
An Electronic Feedback Pressure Regulator
1972
16 pages
Report
No indication
English
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