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Effect of time delay on flying qualities: An updateFlying qualities problems of modern, full-authority electronic flight control systems are most often related to the introduction of additional time delay in aircraft response to a pilot input. These delays can have a significant effect on the flying qualities of the aircraft. Time delay effects are reexamined in light of recent flight test experience with aircraft incorporating new technology. Data from the X-29A forward-swept-wing demonstrator, a related preliminary in-flight experiment, and other flight observations are presented. These data suggest that the present MIL-F-8785C allowable-control system time delay specifications are inadequate or, at least, incomplete. Allowable time delay appears to be a function of the shape of the aircraft response following the initial delay. The cockpit feel system is discussed as a dynamic element in the flight control system. Data presented indicate that the time delay associated with a significant low-frequency feel system does not result in the predicted degradation in aircraft flying qualities. The impact of the feel system is discussed from two viewpoints: as a filter in the control system which can alter the initial response shape and, therefore, the allowable time delay, and as a unique dynamic element whose delay contribution can potentially be discounted by special pilot loop closures.
Document ID
19860018620
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smith, R. E.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Sarrafian, S. K.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-88264
NAS 1.15:88264
H-1351
Report Number: NASA-TM-88264
Report Number: NAS 1.15:88264
Report Number: H-1351
Meeting Information
Meeting: AIAA Guidance
Location: Navigation and Control Conference, Williamsburg, VA
Country: United States
Start Date: August 18, 1986
End Date: August 20, 1986
Accession Number
86N28092
Funding Number(s)
PROJECT: RTOP 505-61
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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