DocumentCode :
622557
Title :
Aircraft control surface failure accommodation utilizing linear regulation and switching control
Author :
Salman, Mishah Uzziel ; Chang, Bo-Yan
Author_Institution :
Dept. of Mech. Eng. & Mech., Drexel Univ., Philadelphia, PA, USA
fYear :
2013
fDate :
12-14 June 2013
Firstpage :
1561
Lastpage :
1566
Abstract :
An actuator jam failure is mitigated using a servomechanism formulation where the failed control surface is modeled as an exogenous input to the degraded plant. The approach exploits switching control, linear output regulation, H2 control theory, and an outer-loop PI control algorithm to track a desired reference input. Application is demonstrated using the nonlinear NASA AirSTAR Generic Transport Model (GTM).
Keywords :
H2 control; PI control; aircraft control; nonlinear control systems; servomechanisms; time-varying systems; GTM; H2 control theory; actuator jam failure mitigation; aircraft control surface failure accommodation; exogenous input; linear output regulation; nonlinear NASA AirSTAR Generic Transport Model; outer-loop PI control algorithm; servomechanism; switching control; Actuators; Aerospace control; Aircraft; Elevators; Equations; Mathematical model; Steady-state;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Automation (ICCA), 2013 10th IEEE International Conference on
Conference_Location :
Hangzhou
ISSN :
1948-3449
Print_ISBN :
978-1-4673-4707-5
Type :
conf
DOI :
10.1109/ICCA.2013.6564984
Filename :
6564984
Link To Document :
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