Hostname: page-component-77c89778f8-m42fx Total loading time: 0 Render date: 2024-07-24T18:06:20.965Z Has data issue: false hasContentIssue false
  • English
  • Français

A Review of Multisensor Fusion Methodologies for Aircraft Navigation Systems

Published online by Cambridge University Press:  19 August 2005

David J. Allerton  and
Huamin Jia
David J. Allerton
Affiliation:
The University of Sheffield. Email: d.j.allerton@sheffield.ac.uk
Huamin Jia
Affiliation:
Cranfield University
Get access Rights & Permissions [Opens in a new window]

Abstract

This paper reviews currently existing fault-tolerant navigation system architectures and data fusion methods used in the design and development of integrated aircraft navigation systems and also compares their advantages and disadvantages. Four fault-tolerant navigation system architectures are reviewed and the associated Kalman filter architectures and algorithms are discussed. These techniques have been used in most integrated aircraft navigation systems. The aim of this review paper is to provide a guide for navigation system designers to develop future aircraft multisensor navigation systems.

Keywords

Data FusionFault ToleranceKalman Filter Architectures
Type
Research Article
Information
The Journal of Navigation , Volume 58 , Issue 3 , September 2005 , pp. 405 - 417
Copyright
© 2005 The Royal Institute of Navigation

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)