NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
F-14 modeling studyPreliminary results in the application of a closed loop pilot/simulator model to the analysis of some simulator fidelity issues are discussed in the context of an air to air target tracking task. The closed loop model is described briefly. Then, problem simplifications that are employed to reduce computational costs are discussed. Finally, model results showing sensitivity of performance to various assumptions concerning the simulator and/or the pilot are presented.
Document ID
19840017633
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Levison, W. H. (Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Baron, S. (Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:172336
NASA-CR-172336
Report Number: NAS 1.26:172336
Report Number: NASA-CR-172336
Accession Number
84N25701
Funding Number(s)
CONTRACT_GRANT: NAS1-16738
PROJECT: RTOP 505-35-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available