NDLI: Adaptive fault compensation for aircraft flight systems with actuator faults

Content Provider	IEEE Xplore Digital Library
Author	Yuying Guo Youmin Zhang Bin Jiang
Copyright Year	2013
Description	Author affiliation: Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China (Bin Jiang) \|\| Dept. of Mech. & Ind. Eng., Concordia Univ., Montreal, QC, Canada (Youmin Zhang) \|\| Sch. of Inf. Eng., Southwest Univ. of Sci. & Technol., Mianyang, China (Yuying Guo)
Abstract	In this paper, an adaptive fault compensation scheme is investigated for aircraft flight systems in the presence of non-measurable rate on the actuator second-order dynamics. The proposed fault compensation scheme is a combination between multiple model and adaptive reconfiguration control. By means of the designed method, the system output can track that of reference model asymptotically, and desired performance of the developed scheme is demonstrated by simulation studies on the lateral dynamic model of a Boeing 747 airplane.
Sponsorship	IEEE Control Syst. Soc.
Starting Page	4921
Ending Page	4926
File Size	173465
Page Count	6
File Format	PDF
ISBN	9781467355339
e-ISBN	9781467355346
DOI	10.1109/CCDC.2013.6561825
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2013-05-25
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Fault Compensation Actuators Adaptation models Multiple Model Atmospheric modeling Educational institutions Actuator Fault Vectors Aircraft Flight Control System
Content Type	Text
Resource Type	Article

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