Integrated Navigation, Guidance, and Control of Missile Systems: 2-D Dynamic Models

Abstract

In this report mathematical models (2-D Azimuth and Elevation Planes) for multi-party engagement kinematics are derived suitable for developing, implementing and testing modern missile guidance systems. The models developed here are suitable for both conventional and more advanced optimal intelligent guidance schemes including those that arise out of the differential game theory. These models accommodate changes in vehicle body attitude and other non-linear effects such as limits on lateral acceleration and aerodynamic forces.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
May 01, 2012
Accession Number
ADA566330

Entities

People

  • Farhan A. Faruqi

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Australia
  • Automatic Pilots
  • Collisions
  • Computational Science
  • Computer Simulations
  • Computers
  • Game Theory
  • Geometry
  • Guidance
  • Mathematical Models
  • Navigation
  • Posture (Physiology)
  • Proportional Navigation
  • Simulations
  • Trajectories
  • Two Dimensional

Readers

  • Control Systems Engineering.
  • Distributed Systems and Data Platform Development
  • Military Science and Technology Research and Modernization.