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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