Angular Motion of Spinning Almost Symmetric Missiles

Abstract

An almost symmetric missile is a missile whose zero-spin pitch and yaw frequencies are 'nearly' equal. The angular motion of a spinning almost symmetric missile can be described by five rotating modal vectors. Two of these vectors vanish when the frequencies are equal. Good approximations for modal frequencies and amplitudes are derived for the special cases of near zero spin and spins near pitch or yaw resonance as well as for spins away from these special regions.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1978
Accession Number
ADA063538

Entities

People

  • Charles H. Murphy

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aeronautical Engineering
  • Angular Momentum
  • Angular Motion
  • Asymmetry
  • Engineering
  • Equations
  • Equations Of Motion
  • Flight
  • Free Flight
  • Frequency
  • Jet Propulsion
  • Military Research
  • Numbers
  • Orientation (Direction)
  • Physics Laboratories
  • Transverse

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.