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Pitch paper pilot revisitedTwo methods are described for predicting the handling qualities of an aircraft in pitch. Both methods are based on minimizing a pilot rating expression with respect to free pilot parameters. In one case the pilot rating expression was developed from a set of moving base simulation data. In the other case, the pilot rating expression was developed from a set of fixed base simulation data. In both cases pilot rating is primarily a function of pitch attitude and pitch rate; however, in the moving base case, the pilot rating is more sensitive to pitch rate than in the fixed base case. For each method, predicted pilot ratings and performance measures agree well with the measured data corresponding to that case. Both methods are used to predict pilot ratings for a set of flight test configurations and the results of the two methods agree to within one half a rating unit. The predicted ratings in both cases correlate well with the actual pilot ratings from the flight tests.
Document ID
19750011061
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Arnold, J. D.
(Air Force Inst. of Tech. Wright-Patterson AFB, OH, United States)
Johnson, R. B., Jr.
(Air Force Inst. of Tech. Wright-Patterson AFB, OH, United States)
Dillow, J. D.
(Air Force Inst. of Tech. Wright-Patterson AFB, OH, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1973
Publication Information
Publication: MIT Proc. of the 9th Ann. Conf. on Manual Control
Subject Category
Aircraft Stability And Control
Accession Number
75N19133
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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