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Terminal guidance systemA terminal guidance system is described including a heading command subsystem and a glide-slope command subsystem which develop command signals for use in guiding an aircraft or other vehicle into a preselected heading and/or altitude at a terminal point. The heading command subsystem is responsive to certain input data and continuously develops command signals for use in directing the aircraft from a remote location to a terminal point so that upon arrival it has a preselected terminal heading. The glide-slope command subsystem is responsive to certain other input data and continuously develops command signals for use in controlling the rate of descent of the aircraft so that it will have a preselected altitude and glide-slope upon arrival at the terminal.
Document ID
19740005307
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Gee, S. W.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 3, 2013
Publication Date
December 4, 1973
Subject Category
Biosciences
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-232021
Patent Number: NASA-CASE-FRC-10049-1
Patent Number: US-PATENT-3,776,455
Accession Number
74N13420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-FRC-10049-1|US-PATENT-3,776,455
Patent Application
US-PATENT-APPL-SN-232021
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