Digital Redesign of Pershing Attitude Control System
Abstract
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 The original PERSHING weapon system attitude control system was implemented by an analogue flight computer which has been replaced by a digital flight computer.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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 29, 1971
- Accession Number
- AD0740648
Entities
People
- Sherman M. Seltzer