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Maximum Normalized Rate as a Flying Qualities ParameterDiscrete attitude commands have become a standard task for flying qualities evaluation and control system testing. Much pilot opinion data is now available for ground-based and in-flight simulations, but adequate performance measures and prediction methods have not been established. The Step Target Tracking Prediction method, introduced in 1978, correlated time-on-target and rms tracking data with NT-33 in-flight longitudinal simulations, but did not employ parameters easily measured in manned flight and simulation. Recent application of the Step Target Tracking Prediction method to lateral flying qualities analysis has led to a new measure of performance. This quantity, called Maximum Normalized Rate (MNR), reflects the greatest attitude rate a pilot can employ during a discrete maneuver without excessive overshoot and oscillation. MNR correlates NT-33 lateral pilot opinion ratings well, and is easily measured during flight test or simulation. Futhermore, the Step Target MNR method can be used to analyze large amplitude problems concerning rate limiting and nonlinear aerodynamics.
Document ID
19850006194
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Onstott, E. D.
(Northrop Corp. Hawthorne, CA, United States)
Warner, J. S.
(Northrop Corp. Hawthorne, CA, United States)
Hodgkinson, J.
(Northrop Corp. Hawthorne, CA, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1984
Publication Information
Publication: NASA. Ames Research Center 20th Ann. Conf. on Manual Control, Vol. 1
Subject Category
Man/System Technology And Life Support
Accession Number
85N14503
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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