Simulink Simulation of Proportional Navigation and Command to Line of Sight Missile Guidance.

Abstract

Proportional Navigation and Command To Line Of Sight missile guidance are explored. A system flow graph is developed for each guidance technique. The block transfer functions are developed and a state space representation of the system is defined. The missile systems are then tested using one two-dimensional engagement and two three-dimensional engagement scenarios. The final three-dimensional scenario introduces measurement noise in order to evaluate the effect of noise on the guidance algorithms. The engagement results are then compared to analyze the miss distance of each type of missile guidance.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1995
Accession Number
ADA298296

Entities

People

  • Patrick Costello

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Algorithms
  • Command Guidance
  • Control Systems
  • Fire Control Systems
  • Geometry
  • Guidance
  • Guided Missiles
  • Line Of Sight
  • Miss Distance
  • Navigation
  • Proportional Navigation
  • Radar
  • Simulations
  • Target Seekers
  • Three Dimensional
  • Transfer Functions
  • Two Dimensional

Readers

  • Computational Modeling and Simulation
  • Computer Vision.
  • Missile Defense Systems.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers