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Simulation development and evaluation of an improved longitudinal velocity vector control wheel steering mode and electronic display formatUsing simulation, an improved longitudinal velocity vector control wheel steering mode and an improved electronic display format for an advanced flight system were developed and tested. Guidelines for the development phase were provided by test pilot critique summaries of the previous system. The results include performances from computer generated step column inputs across the full airplane speed and configuration envelope, as well as piloted performance results taken from a reference line tracking task and an approach to landing task conducted under various environmental conditions. The analysis of the results for the reference line tracking and approach to landing tasks indicates clearly detectable improvement in pilot tracking accuracy with a reduction in physical workload. The original objectives of upgrading the longitudinal axis of the velocity vector control wheel steering mode were successfully met when measured against the test pilot critique summaries and the original purpose outlined for this type of augment control mode.
Document ID
19800021804
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Steinmetz, G. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1980
Subject Category
Aircraft Instrumentation
Report/Patent Number
L-13435
NASA-TP-1664
Report Number: L-13435
Report Number: NASA-TP-1664
Accession Number
80N30305
Funding Number(s)
PROJECT: RTOP 534-04-13-55
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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