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Active control landing gear for ground loads alleviationAn active landing gear has been created by connecting the hydraulic piston in an oleo strut to a hydraulic supply. A controller modulates the pressure in the oleo to achieve the desired dynamic characteristics. Tests on ground rigs (documented by a film) have demonstrated the successful alleviation of induced structural ground loads and the next step will be a flight test using a fighter aircraft.
Document ID
19850018438
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcgehee, J. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Publication Information
Publication: AGARD Tech. Evaluation Rept. on the Flight Mech. Symp. on Active Control Systems
Subject Category
Aircraft Stability And Control
Accession Number
85N26749
Distribution Limits
Public
Copyright
Other
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