Design and Analysis for Early Warning of Rotor UAV Based on Data-Driven DBN

被引:10
作者
Chen, Xue-Mei [1 ]
Wu, Chun-Xue [1 ]
Wu, Yan [2 ]
Xiong, Nai-xue [3 ]
Han, Ren [1 ]
Ju, Bo-Bo [1 ]
Zhang, Sheng [1 ]
机构
[1] Univ Shanghai Sci & Technol, Sch Opt Elect & Comp Engn, Shanghai 200093, Peoples R China
[2] Indiana Univ, ONeill Sch Publ & Environm Affairs, Bloomington, IN 47405 USA
[3] Northeastern State Univ, Dept Math & Comp Sci, Tahlequah, OK 74464 USA
基金
中国国家自然科学基金;
关键词
rotor UAV; data-driven; on-line; early warning; comprehensive fault diagnosis; DBN; FAULT-DIAGNOSIS;
D O I
10.3390/electronics8111350
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The unmanned aerial vehicle (UAV), which is a typical multi-sensor closed-loop flight control system, has the properties of multivariable, time-varying, strong coupling, and nonlinearity. Therefore, it is very difficult to obtain an accurate mathematical diagnostic model based on the traditional model-based method; this paper proposes a UAV sensor diagnostic method based on data-driven methods, which greatly improves the reliability of the rotor UAV nonlinear flight control system and achieves early warning. In order to realize the rapid on-line fault detection of the rotor UAV flight system and solve the problems of over-fitting, limited generalization, and long training time in the traditional shallow neural network for sensor fault diagnosis, a comprehensive fault diagnosis method based on deep belief network (DBN) is proposed. Using the DBN to replace the shallow neural network, a large amount of off-line historical sample data obtained from the rotor UAV are trained to obtain the optimal DBN network parameters and complete the on-line intelligent diagnosis to achieve the goal of early warning as possible as quickly. In the end, the two common faults of the UAV sensor, namely the stuck fault and the constant deviation fault, are simulated and compared with the back propagation (BP) neural network model represented by the shallow neural network to verify the effectiveness of the proposed method in the paper.
引用
收藏
页数:22
相关论文
共 34 条
[1]  
Alkhateeb J.H., 2014, P 2014 6 INT C COMP
[2]  
Altan A., 2017, P 2017 25 SIGN PROC
[3]  
[Anonymous], P IEEE CHIN SUMM INT
[4]  
[Anonymous], P 2014 IEEE 10 INT C
[5]  
Chao Y., 2008, P 2008 27 CHIN CONTR
[6]  
Chen D., 2009, P 2009 5 INT C IM GR
[7]  
Ding S X., 2016, IFAC PAPERSONLINE, V49, P50
[8]  
Ducard G., 2014, P 2014 EUR CONTR C E
[9]   Air data system fault modeling and detection [J].
Freeman, Paul ;
Seiler, Peter ;
Balas, Gary J. .
CONTROL ENGINEERING PRACTICE, 2013, 21 (10) :1290-1301
[10]   UAV Sensor Fault Diagnosis Technology: A Survey [J].
Gao, Yunhong ;
Zhao, Ding ;
Li, Yibo .
ADVANCES IN MANUFACTURING TECHNOLOGY, PTS 1-4, 2012, 220-223 :1833-1837