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Use of Dynamic Distortion to Predict and Alleviate Loss of ControlThis research has developed and evaluated the specific concepts, termed Smart-Cue and Smart-Gain, to alleviate aircraft loss of control that results from unfavorable pilot/vehicle system interactions, including pilot-induced oscillations (PIOs). Unfavorable pilot/ vehicle-system interactions have long been an aviation safety problem. While the effective aircraft dynamic properties involved in these events have been extensively studied and understood, similar scrutiny has not been paid to the many aspects of the primary manual control system that converts the pilot control inputs to motions of the control surfaces. The purpose of the Smart-Cue and Smart-Gain developments is to redress this neglect, and to develop and validate remedial manual control systems.
Document ID
20110012219
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - NASA Tech Brief
Authors
Klyde, David
(Systems Technology, Inc. United States)
Liang, Chi-Ying
(Systems Technology, Inc. United States)
Alvarez, Daniel
(Systems Technology, Inc. United States)
Date Acquired
August 25, 2013
Publication Date
February 1, 2011
Publication Information
Publication: NASA Tech Briefs, February 2011
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-46865
Distribution Limits
Public
Copyright
Public Use Permitted.
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