Integrated Navigation, Guidance, and Control of Missile Systems: 3-D Dynamic Model

Abstract

In this report a 3-D mathematical modelfor multi-party engagement kinematics is derived suitable for developing, implementing and testing modern missile guidance systems. The model developed here is suitable for both conventional and more advanced optimal intelligent guidance schemes including those that arise out of the differential game theory. This model accommodates changes in vehicle body attitude and other non-linear effects such as limits on lateral acceleration and aerodynamic forces.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 2013
Accession Number
ADA584825

Entities

People

  • Farhan A. Faruqi

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

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

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Control Systems Engineering.
  • Inertial Navigation Systems.