A Simulation Study of a Twelve Degree of Freedom System.

Abstract

A twelve degree of freedom model for a missile suspension system was simulated mathematically. The derived equations of motion were solved for missile accelerations and displacements at various driving forces, frequencies, and damping coefficients. The simulation results were validated using measured field data. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1977
Accession Number
ADA044756

Entities

People

  • Eugene B. Hartnett

Organizations

  • Boston College

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Coefficients
  • Coordinate Systems
  • Differential Equations
  • Displacement
  • Equations
  • Equations Of Motion
  • Explosions
  • Frequency
  • Integrals
  • Notation
  • Nuclear Explosions
  • Resonant Frequency
  • Simulations

Readers

  • Computational Modeling and Simulation
  • Control Systems Engineering.