ON THE QUASI-LINEAR SUBSTITUTION METHOD FOR MISSILE MOTION CAUSED BY STRONGLY NONLINEAR STATIC MOMENT

Abstract

An improved quasi-linear substitution method is developed to treat properly the influence of a cubic static moment on the modal damping of a missile acted on by quite general nonlinear damping and Magnus moments. The predictions of this method are compared for various special cases with those of the more accurate but much more complicated perturbation method. The new quasi- linear theory predicts boundary curves for planar motion, almost circular motion and almost planar motion which are quite close to those of the perturbation theory. An original result of the theory is that all planar singular points for a nonspinning missile whose moment coef ficients are only functions of the total angle of attack are nodes. That is, almost planar motion with amplitude close to that of a stable planar limit motion will tend to that motion.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1963
Accession Number
AD0410213

Entities

People

  • Charles H. Murphy

Organizations

  • Ballistic Research Laboratory

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Amplitude
  • Boundaries
  • Differential Equations
  • Engineering
  • Equations
  • Flight
  • Flight Paths
  • Frequency
  • Governments
  • Guided Missiles
  • Integrals
  • Jet Propulsion
  • Mathematics
  • New York
  • Perturbations
  • Physics Laboratories

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Control Systems Engineering.