This paper concerns a new technique designed to provide high performance reaction control systems for sounding rockets. Proportional control of differential thrust and simple adaptive control of thrust magnitude (based on the level of demanded thrust) is utilized. The control is being implemented with a combination of electronic and fluidic components for an Aerobee 150 sounding rocket payload whose goal is a pointing stability of 0.1 arc second.
A New Reaction Control Approach for Sounding Rockets
Sae Technical Papers
National Aeronautic and Space Engineering and Manufacturing Meeting ; 1970
1970-02-01
Aufsatz (Konferenz)
Englisch
A new reaction control approach for sounding rockets
NTRS | 1970
|GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1959
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|Engineering Index Backfile | 1964
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