DocumentCode :
2263335
Title :
Research of UAV fault and state forecast technology based on particle filter
Author :
Baoan, Li ; Zhihua, Liu ; Shufen, Li
Author_Institution :
Beihang Univ., Beijing, China
fYear :
2009
fDate :
14-17 Sept. 2009
Firstpage :
82
Lastpage :
87
Abstract :
This paper presents an UAV fault and state prediction approach which is based on particle filter. In the UAV system, on account of its dynamic environment, mechanical complexity and other factors, it is difficult to avoid all potential faults. So, in order to early detect the potential fault, fault forecast is necessary so as to avoid enormous losses. As the input and output response model of UAV system is nonlinear and multi-parameters, it is need to find an appropriate way to of fault prediction for system maintenance and real-time command. Particle filters are sequential Monte Carlo methods based on point mass (or `particle´) representations of probability densities, which can be applied to any state-space model. Their ability to deal with nonlinear and non-Gaussian statistics makes them suitable for application to the UAV fault prediction. UAV is an extremely complex system, two important aspects of monitoring are focused on this paper: 1) Engine condition monitoring and fault prediction; 2) UAV flight track forecast. The experimental result indicates the effectiveness of this approach.
Keywords :
Monte Carlo methods; aerospace engines; condition monitoring; fault location; filtering theory; maintenance engineering; military aircraft; probability; remotely operated vehicles; sequential estimation; state-space methods; UAV fault; UAV flight track forecast; engine condition monitoring; fault detection; fault forecast; mechanical complexity; particle filter; probability; sequential Monte Carlo methods; state forecast technology; state-space model; system maintenance; unmanned aerial vehicle; Condition monitoring; Fault detection; Nonlinear dynamical systems; Particle filters; Predictive models; Probability; Real time systems; Statistics; Technology forecasting; Unmanned aerial vehicles; UAV; cylinder head temperature; engine speed; fault prediction; flight track; particle filter; pitch angle; roll angle;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
AUTOTESTCON, 2009 IEEE
Conference_Location :
Anaheim, CA
ISSN :
1088-7725
Print_ISBN :
978-1-4244-4980-4
Electronic_ISBN :
1088-7725
Type :
conf
DOI :
10.1109/AUTEST.2009.5314050
Filename :
5314050
Link To Document :
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