Combined Satellite and Inertial Navigation Systems can achieve extremely high positioning accuracies in the sub meter range even in the dynamic environment of aircraft. This paper presents the concept of the 'Integrated Navigation System' developed at the Institute of Flight Guidance using coupled satellite and inertial sensors. Flight test results are shown, which demonstrate that this system has the potential to achieve the accuracy requirements according to ICAO CAT 3 for high precision approaches even under bad weather conditions.
Integrated Precision Navigation System
1992
10 pages
Report
Keine Angabe
Englisch
British Library Conference Proceedings | 2006
|High Precision Integrated Navigation System for Vehicle Guidance
British Library Conference Proceedings | 1999
|Low Cost Inertial Sensors for Precision Navigation in Integrated Satellite-/Inertial Navigation
British Library Conference Proceedings | 1994
|High-precision Mars Entry Integrated Navigation Under Large Uncertainties
Online Contents | 2014
|