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Identification of pilot dynamics from in-flight tracking dataData from a representative flight task involving an F-14 'pursuer' aircraft tracking a T-38 'target' aircraft in a 3G wind-up turn and in level flight are processed using a least squares identification technique in an attempt to identify pilot/vehicle dynamics. Comparative identification results are provided by a Fourier coefficient method which requires a carefully designed and implemented input consisting of a sum of sinusoids. The least-squares results compare favorably with those obtained by the Fourier technique. An example of crossover frequency regression is discussed in the light of the conditions of one of the flight configurations.
Document ID
19850063784
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hess, R. A.
(California, University Davis, United States)
Mnich, M. A.
(California Univ. Davis, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 85-1945
Meeting Information
Meeting: Guidance, Navigation and Control Conference
Location: Snowmass, CO
Start Date: August 19, 1985
End Date: August 21, 1985
Accession Number
85A45935
Distribution Limits
Public
Copyright
Other

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