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The 4D-TECS integration for NASA TSRV airplaneThe integration of the Total Energy Control System (TECS) concept with 4D navigation is described. This integration was made to increase the operational capacity of modern aircraft and encourage incorporation of this increased capability with the evolving National Airspace System (NAS). Described herein is: 4D smoothing, the basic concepts of TECS, the spoiler integration concept, an algorithm for nulling out time error, speed and altitude profile modes, manual spoiler implementation, 4D logic, and the results of linear and nonlinear analysis.
Document ID
19890014100
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kaminer, I. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Oshaughnessy, P. R. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1989
Publication Information
Publisher: NASA
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-4231
NAS 1.26:4231
Report Number: NASA-CR-4231
Report Number: NAS 1.26:4231
Accession Number
89N23471
Funding Number(s)
CONTRACT_GRANT: NAS1-18027
PROJECT: RTOP 505-55-41-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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