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Aircraft roll steering command systemAircraft roll command signals are generated as a function of the Microwave Landing System based azimuth, groundtrack, groundspeed and azimuth rate or range distance input parameters. On initial approach, roll command signals are inhibited until a minimum roll command requirement is met. As the aircraft approaches the centerline of the runway, the system reverts to a linear track control.
Document ID
20080007402
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Lambregts, Antonius A.
Date Acquired
August 24, 2013
Publication Date
August 6, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-294274
Patent Number: US-PATENT-4,533,999
Funding Number(s)
CONTRACT_GRANT: NAS1-14880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,533,999
Patent Application
US-PATENT-APPL-SN-294274
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