NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Langley Research Center contributions in advancing active control technologyThe application of active control technology to reduce aeroelastic response of aircraft structures offers a potential for significant payoffs in terms of aerodynamic efficiency and weight savings. Some of the contributions of the Langley Research Center in advancing active control technology are described. Contributions are categorized into the development of appropriate analysis tools, control law synthesis methodology, and experimental investigations aimed at verifying both analysis and synthesis methodology.
Document ID
19810010476
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abel, I. (NASA Langley Research Center Hampton, VA, United States)
Newsom, J. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: Advan. Aerodyn. and Active Controls
Subject Category
Aircraft Stability And Control
Accession Number
81N19002
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19810010475Collected WorksAdvanced aerodynamics and active controls. Selected NASA research
No Preview Available