Assessment of a Dynamical Gyroscope Model Utilizing Digital Simulation Techniques

Abstract

This report presents an assessment and performance of a dynamical gyroscope modelled for a six-degree-of-freedom digital missile trajectory simulation. Mathematical models and digital simulation results of an idealized gyro model and the dynamical (realistic) model are given. The computer program listings are presented in the appendices. (AUthor)

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Document Details

Document Type
Technical Report
Publication Date
Jun 03, 1977
Accession Number
ADA042497

Entities

People

  • Larry R. Murdock

Organizations

  • United States Army Aviation and Missile Command

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Angular Momentum
  • Artillery
  • Command And Control
  • Command Control Communications
  • Computer Programs
  • Conductive Polymers
  • Control Systems
  • Control Systems Engineering
  • Coordinate Systems
  • Differential Equations
  • Equations
  • Euler Angles
  • Guidance
  • Molecular Dynamics
  • Plastic Explosives
  • Proportional Navigation
  • Simulations

Readers

  • Computational Modeling and Simulation
  • Control Systems Engineering.