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Flight simulation for wind shear encounterA real-time piloted flight simulator is under development in the Laboratory for Control and Automation at Princeton University. This facility will be used to study piloted flight through a simulated wind shear. It will also provide a testbed for real-time flight guidance laws. The hardware configuration and aerodynamic model used are discussed. The microburst model to be incorporated into the simulation is introduced, and some proposed cockpit display concepts are described.
Document ID
19910009722
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mulgund, Sandeep S.
(Princeton Univ. NJ, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1990
Publication Information
Publication: NASA, Langley Research Center, Joint University Program for Air Transportation Research, 1989-1990
Subject Category
Research And Support Facilities (Air)
Accession Number
91N19035
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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