NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A summary of the application of active controls technology in the ATT system studiesThe application of active controls technology to subsonic, long-range transport aircraft was investigated in three Advanced Transport Technology system studies. Relaxed stability requirements, maneuver and gust load alleviation, and active flutter suppression were the concepts considered. A different configuration was investigated for each of the three airframe manufacturers, and each had a somewhat different approach to the application of active controls technology. Consequently, the results varied in magnitude between the contractors, but several trends were noted. Relaxed stability requirements resulted in the largest benefits - reduced weight, increased return on investment, and decreased direct operating costs. Maneuver load alleviation, gust load alleviation, and flutter suppression resulted in much smaller benefits. Prior to application of active controls technology, a research and development program directed toward fulfilling data base requirements, establishing effective design techniques and criteria, improving systems maintainability and reliability, and demonstrating technology readiness must be completed.
Document ID
19760024072
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hood, R. V.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N31160
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available