DocumentCode :
2707423
Title :
An improved method for risk assessment of carrier-based aircraft
Author :
Zhu, Qidan ; Li, Hui ; Zhang, Zhi ; Wang, Lipeng
Author_Institution :
Dept. of Autom., Harbin Eng. Univ., Harbin, China
fYear :
2012
fDate :
6-8 June 2012
Firstpage :
777
Lastpage :
782
Abstract :
During the process of aircraft landing, the risk assessment of pilot control characteristics is always used to predict aircraft safety. This is one of the important methods to avoid pilot-aircraft adverse coupling. In order to keep the accuracy of the assessment result, this paper presents an improved method for defining the landing risk assessment using Safe Flight Area during approach. This area which links with the aircraft states is established and introduced in a control scheme using closed-loop pilot-aircraft system which is evaluated by flying qualities. The risk assessment results indicate the better performance of the new method with more accuracy and practicability in comparison with the traditional LSO subjective decisions.
Keywords :
aerospace safety; aircraft control; closed loop systems; risk management; LSO subjective decisions; aircraft landing; aircraft safety; carrier-based aircraft; closed-loop pilot-aircraft system; pilot control characteristics; pilot-aircraft adverse coupling; risk assessment; safe flight area; Aerospace control; Aircraft; Atmospheric modeling; Integrated circuits; Mathematical model; Risk management; Trajectory; Closed-Loop Pilot-Aircraft System; Flying Qualities; Risk Assessment; Safe Flight Area;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Information and Automation (ICIA), 2012 International Conference on
Conference_Location :
Shenyang
Print_ISBN :
978-1-4673-2238-6
Electronic_ISBN :
978-1-4673-2236-2
Type :
conf
DOI :
10.1109/ICInfA.2012.6246924
Filename :
6246924
Link To Document :
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