NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Ride-quality testing under controlled flight conditionsAs part of a NASA program to develop the technology of ride quality, a flight-test program has been conducted to obtain subjective reactions of a significant number of test passengers to a variety of controlled and repeatable flight conditions. For these experiments, the computer of a variable-stability research aircraft was programmed to precisely control the aircraft's in-flight motions as specified by motion command signals prerecorded on magnetic tape. Problems initially encountered derived primarily from the quality of the motion command signals and tape playback device, plus the aircraft motion response in degrees of freedom other than that desired. Problem solutions were obtained through the use of filtering and compensating networks. The variable-stability-system modifications, problems encountered, and their solutions are described. The test procedure is described and sample results are presented which illustrate the usefulness of this technique for ride-quality research.
Document ID
19750055430
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schoonover, W. E., Jr.
(NASA Langley Research Center Hampton, Va., United States)
Dittenhauser, J.
(Calspan Corp. Buffalo, N.Y., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 75-987
Report Number: AIAA PAPER 75-987
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting
Location: Los Angeles, CA
Start Date: August 4, 1975
End Date: August 7, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A39502
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available