A Study of Multiloop Feedback Flight Control System Having a Positive Effect on Pilot-Induced Oscillation (PIO)

A Study of Multiloop Feedback Flight Control System Having a Positive Effect on Pilot-Induced Oscillation (PIO)

The focus of this study is on PIO to be solved in the development of modern flight control systems. Especially, it is important to investigate the fully-developed PIO as a worst case for the safety of piloted airplanes and to analyze the limit cycle phenomenon including the effects of actuator rate...

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Veröffentlicht in:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2004, Vol.52(601), pp.51-56
1. Verfasser: Katayanagi, Ryoji
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Sprache:eng ; jpn
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Feedback Control
PIO
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description The focus of this study is on PIO to be solved in the development of modern flight control systems. Especially, it is important to investigate the fully-developed PIO as a worst case for the safety of piloted airplanes and to analyze the limit cycle phenomenon including the effects of actuator rate limiting and feedback control loop. Lateral-directional flight control system was taken for instance, this paper proposes a technique to design the feedback control law to have a positive effect on PIO to decrease the amplitude of the oscillation.
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source Elektronische Zeitschriftenbibliothek - Frei zugängliche E-Journals
subjects Feedback Control
PIO
title A Study of Multiloop Feedback Flight Control System Having a Positive Effect on Pilot-Induced Oscillation (PIO)
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