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Results of aircraft open-loop tests of an experimental magnetic leader cable system for guidance during roll-out and turnoffAn experimental magnetic leader cable (MLC) system designed to measure aircraft lateral displacement from centerline and heading relative to centerline during rollout, turnoff, and taxi was tested at NASA's Wallops Flight Facility using NASA's Transport System Research Vehicle (TSRV), a modified B-737. The MLC system consisted of ground equipment that produced a magnetic field about a wire along runway centerline and airborne equipment that detected the strength and direction of this field and computed displacement and heading. Results of these tests indicate that estimates of aircraft displacement from centerline produced by the magnetic leader cable system using either of the two algorithms appear to be adequate for use by an automatic control system during rollout, turnoff, and taxi. Estimates of heading, however, are not sufficiently accurate for use, probably because of distortion of the magnetic field by the metal aircraft.
Document ID
19900007451
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bundick, W. Thomas
(NASA Langley Research Center Hampton, VA, United States)
Middleton, David B.
(NASA Langley Research Center Hampton, VA, United States)
Poole, William L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-4135
NAS 1.15:4135
L-16574
Report Number: NASA-TM-4135
Report Number: NAS 1.15:4135
Report Number: L-16574
Accession Number
90N16767
Funding Number(s)
PROJECT: RTOP 505-66-41-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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