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
1978-09-01
Report
No indication
English
Optimal Design of Robust Analytical Redundancy for Redundant Strapdown Inertial Navigation System
British Library Conference Proceedings | 1997
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