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Strapdown system redundancy management flight demonstrationThe 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.
Document ID
19780024136
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA-CR-145356
Report Number: NASA-CR-145356
Accession Number
78N32079
Funding Number(s)
CONTRACT_GRANT: NAS1-15155
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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