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A theoretical investigation of the influence of autopilot natural frequency upon the dynamic performance characteristics of a supersonic canard missile configuration with a pitch-attitude control system
Author:
Passera, Anthony L
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51H02
Link:
https://digital.library.unt.edu/ark:/67531/metadc58918/
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