Kalman Filter Integration of Modern Guidance and Navigation Systems

Abstract

The integration of modern guidance and navigation systems is usually performed with a sub-optimal implementation when considering system modelling, algorithm design and real hardware non-linearities. This lecture series brings together a group of speakers with outstanding practical experience in the design of integrated systems, providing the audience with the principles, insights and mechanisms of real, current-day system synthesis approaches and giving the overall background necessary for synthesizing future practical guidance and navigation systems. Two of the lectures deal with the synthesis of solutions to tracking problems. The remainder of the lectures deal with the integration of avionics systems.

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Document Details

Document Type
Technical Report
Publication Date
Jul 04, 1989
Accession Number
ADA214284

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Ground and Sea Platforms
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Computational Science
  • Computer Programming
  • Computer Programs
  • Control Systems
  • Dead Reckoning
  • Detection
  • Geometry
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Kalman Filters
  • Mathematical Filters
  • Measurement
  • Navigation
  • Three Dimensional
  • World Geodetic System

Fields of Study

  • Computer science

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Inertial Navigation Systems.
  • Military History / Militaries and War Studies