NDLI: Key technology research on fault detection and diagnosis for broken-wing small unmanned aerial vehicle

Content Provider	IEEE Xplore Digital Library
Author	Huang Junjie Jiang Zhen Li Shuping Xu Xinli Shi Xiaobin
Copyright Year	2012
Description	Author affiliation: Department of Mechatronics Engineering and Automation, Shanghai University, China (Huang Junjie; Jiang Zhen; Li Shuping; Xu Xinli; Shi Xiaobin)
Abstract	An accident with any component failure of the small unmanned aerial vehicle (SUAV) will happen in the operation process. At present the sensor and actuator faults are mostly studied and the damaged body considers very few. The research status of the air dynamics and fault detection and diagnosis (FDD) are firstly introduced in the paper. The methods of the pneumatic parameters and properties on the broken-wing SUAV and the key technologies of FDD are analyzed. At last the experiment of the broken-wing SUAV is established by using the FDD subsystems. A specific plan and research methods is provided through the paper. Meanwhile it provides the theory and research foundation for reconstruction control system.
Starting Page	3049
Ending Page	3052
File Size	143498
Page Count	4
File Format	PDF
ISBN	9781467313971
e-ISBN	9781467313988
DOI	10.1109/WCICA.2012.6358394
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-07-06
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aerodynamics Fault diagnosis Mathematical model Control systems Nonlinear systems Vehicles Educational institutions Identification method Broken-wing SUAV Pneumatic parameters FDD
Content Type	Text
Resource Type	Article

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