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Terminal area automatic navigation, guidance, and control 1: Automatic rollout, turnoff, and taxisA study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader cable signals and develop breaking and reverse thrust guidance laws to provide for rapid automated rollout, turnoff, and taxi to reduce runway occupation time for a wide variety of landing conditions for conventional commercial-type aircraft, is described. Closed loop guidance laws for braking and reverse thrust are derived for rollout, turnoff, and taxi, as functions of the landing speed, the desired taxi speed and the distance to go. Brake limitations for wet runway conditions and reverse thrust limitations are taken into account to provide decision rules to avoid tire skid and to choose an alternate turnoff point, farther down the runway, to accommodate extreme landing conditions.
Document ID
19810022682
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
August 1, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-3451
AMA-80-1
Report Number: NASA-CR-3451
Report Number: AMA-80-1
Accession Number
81N31224
Funding Number(s)
CONTRACT_GRANT: NAS1-15116
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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