Simulation study of three instrument displays to assist in airplane thrust management

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086 0 ‡aNAS 1.14:D-5982
088 ‡aNASA-TN-D-5982
100 1 ‡aMcLaughlin, Milton D.
245 1 0 ‡aSimulation study of three instrument displays to assist in airplane thrust management ‡h[electronic resource] / ‡cMilton D. McLaughlin.
246 3 ‡aNASA TN D-5982
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], ‡c1970.
300 ‡a43 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vD-5982
504 ‡aIncludes bibliographical references (p. 23).
520 ‡aThree displays were evaluated on a piloted simulator, each of which provided information which could be used in thrust management. The three displays were (1) rate of change of speed, (2) potential flight-path angle, and (3) potential rate of climb. Results are presented in the form of time histories, histograms, and pilot comments. The results include comparisons of flight-path and speed control and throttle activity with and without each display and pilot comments.
538 ‡aMode of access: Internet.
538 ‡aSystem requirements: Adobe Acrobat Reader.
538 ‡aMode of access: World Wide Web.
650 0 ‡aAirplanes ‡xMotors ‡xThrust.
710 2 ‡aLangley Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011444202
DAT 0 ‡a20101109150628.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-14T18:25:49Z
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