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Interpreting the handling qualities of aircraft with stability and control augmentationThe general process of designing an aircraft for good flying qualities is first discussed. Lessons learned are pointed out, with piloted evaluation emerging as a crucial element. Two sources of rating variability in performing these evaluations are then discussed. First, the finite endpoints of the Cooper-Harper scale do not bias parametric statistical analyses unduly. Second, the wording of the scale does introduce some scatter. Phase lags generated by augmentation systems, as represented by equivalent time delays, often cause poor flying qualities. An analysis is introduced which allows a designer to relate any level of time delay to a probability of loss of aircraft control. This view of time delays should, it is hoped, allow better visibility of the time delays in the design process.
Document ID
19910031662
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hodgkinson, J.
(Douglas Aircraft Co., Inc. Long Beach, CA, United States)
Potsdam, E. H.
(Douglas Aircraft Co. Long Beach, CA, United States)
Smith, R. E.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 90-2825
Accession Number
91A16285
Distribution Limits
Public
Copyright
Other

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