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Terminal area automatic navigation, guidance, and control research using the Microwave Landing System (MLS). Part 4: Transition path reconstruction along a straight line path containing a glideslope change waypointThe necessary algorithms to reconstruct the glideslope change waypoint along a straight line in the event the aircraft encounters a valid MLS update and transition in the terminal approach area are presented. Results of a simulation of the Langley B737 aircraft utilizing these algorithms are presented. The method is shown to reconstruct the necessary flight path during MLS transition resulting in zero cross track error, zero track angle error, and zero altitude error, thus requiring minimal aircraft response.
Document ID
19820020393
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pines, S.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1982
Publication Information
Publisher: NASA
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA-CR-3574
AMA-81-37
NAS 1.26:3574
Report Number: NASA-CR-3574
Report Number: AMA-81-37
Report Number: NAS 1.26:3574
Accession Number
82N28269
Funding Number(s)
CONTRACT_GRANT: NAS1-15116
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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