Accession Number:

ADA214284

Title:

Kalman Filter Integration of Modern Guidance and Navigation Systems

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1989-07-04

Pagination or Media Count:

190.0

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.

Subject Categories:

  • Computer Programming and Software
  • Air Navigation and Guidance

Distribution Statement:

APPROVED FOR PUBLIC RELEASE