The suitability of strapdown inertial systems in providing highly reliable short-term navigation for vertical take-off and landing (VTOL) aircraft operating in an intra-urban setting under all-weather conditions was assessed. A preliminary design configuration of a skewed sensor inertial reference system employing a redundancy management concept to achieve fail-operational, fail-operational performance, was developed.
Strapdown System Redundancy Management Flight Demonstration
1978
73 pages
Report
No indication
English
Optimal Design of Robust Analytical Redundancy for Redundant Strapdown Inertial Navigation System
British Library Conference Proceedings | 1997
|