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A study for active control research and validation using the Total In-Flight Simulator (TIFS) aircraftThe results of a feasibility study and preliminary design for active control research and validation using the Total In-Flight Simulator (TIFS) aircraft are documented. Active control functions which can be demonstrated on the TIFS aircraft and the cost of preparing, equipping, and operating the TIFS aircraft for active control technology development are determined. It is shown that the TIFS aircraft is as a suitable test bed for inflight research and validation of many ACT concepts.
Document ID
19750011199
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chen, R. T. N. (Calspan Corp. Buffalo, NY, United States)
Daughaday, H. (Calspan Corp. Buffalo, NY, United States)
Andrisani, D., II (Calspan Corp. Buffalo, NY, United States)
Till, R. D. (Calspan Corp. Buffalo, NY, United States)
Weingarten, N. C. (Calspan Corp. Buffalo, NY, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1975
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AK-5560-F-1
NASA-CR-132614
Report Number: AK-5560-F-1
Report Number: NASA-CR-132614
Accession Number
75N19271
Funding Number(s)
CONTRACT_GRANT: NAS1-13329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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