NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flying qualities criteria and flight control designDespite the application of sophisticated design methodology, newly introduced aircraft continue to suffer from basic flying qualities deficiencies. Two recent meetings, the DOD/NASA Workshop on Highly Augmented Aircraft Criteria and the NASA Dryden Flight Research Center/Air Force Flight Test Center/AIAA Pilot Induced Oscillation Workshop, addressed this problem. An overview of these meetings is provided from the point of view of the relationship between flying qualities criteria and flight control system design. Among the items discussed are flying qualities criteria development, the role of simulation, and communication between flying qualities specialists and control system designers.
Document ID
19810059723
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Berry, D. T.
(NASA Flight Research Center Edwards AFB, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 81-1823
Meeting Information
Meeting: Guidance and Control Conference
Location: Albuquerque, NM
Start Date: August 19, 1981
End Date: August 21, 1981
Accession Number
81A44127
Distribution Limits
Public
Copyright
Other

Available Downloads

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