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Evaluation of HiMAT aircraft landing approach lateral control gearing using simulation and a visual displayThe utility of a visual display when studying the influence of changes in lateral stick gearing gains on the Highly Maneuverable Aircraft Technology (HiMAT) vehicle handling qualities during simulated approaches and landings is investigated. The visual display improved the validity of the simulation and provided improved roll response cues for the HiMAT aircraft landing approach. A range of acceptable constant lateral stick gearing gains is found that provides adequate maneuverability and allows for precision moments.
Document ID
19840019675
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sarrafian, S. K. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:84916
H-1205
NASA-TM-84916
Report Number: NAS 1.15:84916
Report Number: H-1205
Report Number: NASA-TM-84916
Accession Number
84N27743
Funding Number(s)
PROJECT: RTOP 533-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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