NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Aircraft landing control systemUpon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertical acceleration are generated as functions of aircraft position and velocity with respect to the ground. The command signals are compared with corresponding actual values to generate error signals which are used to control the flight path.
Document ID
20080004210
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Lambregts, Antonius A.
Hansen, Rolf
Date Acquired
August 24, 2013
Publication Date
November 2, 1982
Subject Category
Aircraft Stability And Control
Report/Patent Number
Patent Number: US-PATENT-4,357,661
Patent Application Number: US-PATENT-APPL-SN-123529
Funding Number(s)
CONTRACT_GRANT: NAS1-14880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,357,661
Patent Application
US-PATENT-APPL-SN-123529
No Preview Available