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Flight evaluation of height response characteristics for the hover bob-up task and comparison with proposed criteriaThe CH-47B variable-stability helicopter was used to evaluate a range of height-response configurations while performing a precision hover bob-up task. The purpose of the study was to assess the validity of results obtained in previous ground-based and in-flight simulations in the context of a precision bob-up task and to provide additional flight data for inclusion in revisions to specifications for helicopter handling qualities. Height response characteristics were implemented using explicit model-following techniques, and the resulting CH-47B dynamics were validated using time-domain and frequency-domain data-analysis methods. The tests complemented the previous investigations by providing detailed pilot comments and ratings, and performance and control-utilization data that relate exclusively to the hover bob-up task. The results are compared with those from previous investigations and with new criteria that have been proposed for handling qualities requirements for helicopters.
Document ID
19870031981
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hindson, W. S.
(NASA Stanford University Joint Institute of Aeronautics and Acoustics, CA, United States)
Tucker, G. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Lebacqz, J. V.
(NASA Ames Research Center Moffett Field, CA, United States)
Hilbert, K. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Accession Number
87A19255
Distribution Limits
Public
Copyright
Other

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