Damage-tolerant Control System Design for Propulsion-controlled Aircraft

Damage-tolerant Control System Design for Propulsion-controlled Aircraft

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This thesis presents a damage-tolerant flight control system design for propulsion-controlled aircraft (PCA). PCA refers to an emergency piloting strategy that flight crews use throttle modulation only to achieve the attitude control of aircraft in case of conventional flight control system failures...

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Bibliographic Details
Main Author: Hitachi, Yoshitsugu
Other Authors: Liu, Hugh
Language:en_ca
Published: 2009
Subjects:
aerospace engineering
control engineering
aircraft flight control
0538
Online Access:http://hdl.handle.net/1807/18342

Internet

http://hdl.handle.net/1807/18342

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