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Research on reconfiguration design of flight controller bas..:

, In: CSAA/IET International Conference on Aircraft Utility Systems (AUS 2022),

Qu, Q. ; Wang, H. ; Li, T.. - p. None , 2022

Link: https://doi.org/10.1049/icp.2022.1553

RT 
T1 <cTitle>CSAA/IET International Conference on Aircraft Utility Systems (AUS 2022)</cTitle>: T1 <Title>Research on reconfiguration design of flight controller based on control allocation under actuator failure</Title>

UL https://suche.suub.uni-bremen.de/peid=ieee-9946073&Exemplar=1&LAN=DE
				
A1 Qu, Q.
A1 Wang, H.
A1 Li, T.
A1 Gu, F.
YR 2022
K1 actuators
K1 aerospace control
K1 aircraft control
K1 control system synthesis
K1 nonlinear control systems
K1 redundancy
K1 reconfiguration design
K1 actuator failure
K1 flight control performance
K1 multicontrol surface aircraft control redundancy
K1 flight controller design strategy
K1 traditional control law module
K1 three-axis control commands
K1 control allocation module
K1 multicontrol surfaces
K1 flight quality
K1 flight reconfiguration controller
K1 original control law
K1 remaining normal control surfaces
SP None
LK http://dx.doi.org/https://doi.org/10.1049/icp.2022.1553
DO https://doi.org/10.1049/icp.2022.1553
SF ELIB - SuUB Bremen

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