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Application of active control technology to aircraft ride smoothingPrototype Ride Smoothing System (RSSs) were synthesized for flight testing aboard the National Aeronautics and Space Administration General Purpose Airborne Simulator (GPAS). The systems were designed to meet comprehensive criteria including passenger comfort and aircraft handling qualities considerations. System performance estimates based on analytic expressions were compared to estimates derived from digital calculations. The effect of RSSs on pilot workload during ILS approach in turbulence was examined in a fixed-base simulator. A limited number of flights were conducted to verify predicted RSS performance. Results of these experiments indicate that RSSs reduce pilot workload and increase passenger comfort while maintaining handling qualities.
Document ID
19750055452
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jacobson, I. D.
Lapins, M.
(Virginia, University Charlottesville, Va., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 75-1029
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
75A39524
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-202
Distribution Limits
Public
Copyright
Other

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