In the report the revised technique for designing a tactical rocket attitude control system has been extended and applied to the redesign of a continuous control system. The original PERSHING weapon system attitude control system was implemented by an analogue flight computer which has been replaced by a digital flight computer. The report presents a design technique for designing a digital attitude control system for the PERSHING weapon system. The design goal is to match the digital system response to that of the original analogue system. (Author)
Digital Redesign of Pershing Attitude Control System
1971
20 pages
Report
Keine Angabe
Englisch
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