[1]郑佳静,李平.采用滑模观测器的四旋翼无人机执行器加性故障容错控制[J].华侨大学学报(自然科学版),2019,40(4):437-443.[doi:10.11830/ISSN.1000-5013.201810019]
 ZHENG Jiajing,LI Ping.Fault Tolerant Control of Actuator Additive Fault for Quadrotor Using Sliding Mode Observer[J].Journal of Huaqiao University(Natural Science),2019,40(4):437-443.[doi:10.11830/ISSN.1000-5013.201810019]
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采用滑模观测器的四旋翼无人机执行器加性故障容错控制()
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《华侨大学学报(自然科学版)》[ISSN:1000-5013/CN:35-1079/N]

卷:
第40卷
期数:
2019年第4期
页码:
437-443
栏目:
出版日期:
2019-07-10

文章信息/Info

Title:
Fault Tolerant Control of Actuator Additive Fault for Quadrotor Using Sliding Mode Observer
文章编号:
1000-5013(2019)04-0437-07
作者:
郑佳静 李平
华侨大学 信息科学与工程学院, 福建 厦门 361021
Author(s):
ZHENG Jiajing LI Ping
College of Information Science and Engineering, Huaqiao University, Xiamen 361021, China
关键词:
四旋翼无人机 容错控制 加性故障 滑模观测器 反步法
Keywords:
quadrotor fault tolerant control additive fault sliding mode observer backstepping method
分类号:
V249.122.3;TP302.8
DOI:
10.11830/ISSN.1000-5013.201810019
文献标志码:
A
摘要:
为了获得四旋翼无人机更好的飞行性能,在考虑外界干扰的情况下,基于滑模观测器对四旋翼无人机的执行器故障问题进行容错控制设计.首先,针对受干扰和发生执行器故障的四旋翼无人机进行建模;然后,设计一种滑模观测器重构故障信息,并实时估计外界扰动;最后,基于观测所得信号,采用反步法设计内环姿态控制器和外环位置控制器,实现故障容错和干扰补偿,保证四旋翼无人机稳定跟踪既定轨迹.仿真结果验证了所提方案的有效性.
Abstract:
In order to obtain better flight performance of quadrotor, considering the situation of external disturbance, fault tolerant control design was conducted based on sliding mode observer for the problem of quadrotor’s actuator fault. First, the model of quadrotor with the effects of disturbances and faults was built. Then, a kind of sliding mode observer was designed to reconstruct the fault information and estimate the external disturbances in real time. Finally, based on the obtained observation signals, the backstepping algorithm was used to design attitude controllers for the inner loop and the position controller for the outer loop to realize fault tolerance and disturbance compensation, which ensured that the quadrotor can track the desired trajectory stably. Simulation results proved the effectiveness of the proposed scheme.

参考文献/References:

[1] 黄志伟,徐苏楠,韦一,等.STM32的多传感器融合姿态检测[J].华侨大学学报(自然科学版),2015,36(4):422-426.DOI:10.11830/ISSN.1000-5013.2015.04.0422.
[2] 张益鹏.四旋翼无人机自适应控制与故障容错[D].南京:南京邮电大学,2014.
[3] 范佳明.四旋翼飞行器容错控制研究[D].天津:天津工业大学,2017.
[4] 贺有智,刘同其.四旋翼飞行器时延积分反演容错控制[J].系统工程与电子技术,2015,37(10):2341-2346.DOI:10.3969/j.issn.1001-506X.2015.10.23.
[5] 韩业壮,华容.四旋翼飞行器的RBF网络自适应滑模控制[J].电光与控制,2017,24(11):22-27.DOI:10.3969/j.issn.1671-637x.2017.11.005.
[6] 魏青铜,陈谋,吴庆宪.输入饱和与姿态受限的四旋翼无人机反步姿态控制[J].控制理论与应用,2015,32(10):1361-1369.DOI:10.7641/CTA.2015.50476.
[7] 吴丽娜,张迎春,赵石磊,等.滑模观测器在卫星姿控系统故障诊断中的应用[J].哈尔滨工业大学学报,2011,43(9):14-18.DOI:10.11918/j.issn.0367-6234.2011.09.003.
[8] 穆凌霞,余翔,李平,等.自适应广义滑模观测器之状态估计和故障重构[J].控制理论与应用,2017,34(4):483-490.DOI:10.7641/CTA.2017.60744.
[9] 朱芳来,李志强.非线性系统执行器故障检测及重构[J].同济大学学报(自然科学版),2013,41(7):1106-1111.DOI:10.3969/j.issn.0253-374x.2013.07.025.
[10] LAN Jianglin,PATTON R J,PUNTA E.Fault-tolerant tracking control for a 3-DOF helicopter with actuator faults and saturation[J].IFAC-PapersOnLine,50(1):5250-5255.DOI:10.1016/j.ifacol.2017.08.465.
[11] 侯明冬,刘金琨,田杰.欠驱动四旋翼飞行器全局轨迹跟踪滑模控制[J].控制工程,2016,23(6):928-932.DOI:10.14107/j.cnki.kzgc.150611.
[12] 王大伟,高席丰.四旋翼无人机滑模轨迹跟踪控制器设计[J].电光与控制,2016(7):55-58.DOI:10.3969/j.issn.1671-637x.2016.07.012.
[13] ZHENG Enhui,XIONG Jingjing,LUO Jiliang.Second order sliding mode control for a quadrotor UAV[J].ISA Transactions,2014,53(4):1350-1356.DOI:10.1016/j.isatra.2014.03.010.
[14] BHATKHANDE P,HAVENS T C.Real time fuzzy controller for quadrotor stability control[C]//IEEE International Conference on Fuzzy Systems.Beijing:IEEE Press,2014:913-919.DOI:10.1109/FUZZ-IEEE.2014.6891787.
[15] 李一波,宋述锡.基于模糊自整定PID四旋翼无人机悬停控制[J].控制工程,2013,20(5):910-914.DOI:10.3969/j.issn.1671-7848.2013.05.028.
[16] 李砚浓,李汀兰,姜艺,等.基于RBF神经网络自适应PID四旋翼飞行器控制[J].控制工程,2016,23(3):378-382.DOI:10.14107/j.cnki.kzgc.150303.
[17] 聂博文.微小型四旋翼无人直升机建模及控制方法研究[D].长沙:国防科学技术大学,2006.
[18] 滕雄,吴怀宇,陈洋,等.基于反步法的四旋翼飞行器轨迹跟踪研究[J].计算机仿真,2016,33(5):78-83.DOI:10.3969/j.issn.1006-9348.2016.05.017.
[19] ZHANG Zhuo,LIU Zhenghua,WEN Nuan.Research on adaptive backstepping sliding mode control method for a hex-rotor Unmanned Aerial Vehicle[C]//IEEE Chinese Guidance, Navigation and Control Conference.Nanjing:IEEE Press,2017:547-552.DOI:10.1109/CGNCC.2016.7828844.
[20] XIONG Jingjing,ZHANG Guobao.Global fast dynamic terminal sliding mode control for a quadrotor UAV[J].ISA Transactions,2016,66:233.DOI:10.1016/j.isatra.2016.09.019.

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备注/Memo

备注/Memo:
收稿日期: 2018-10-09
通信作者: 李平(1981-),女,副教授,博士,主要从事非线性系统与先进控制、容错控制系统的研究.E-mail:pingping_1213@126.com.
基金项目: 国家自然科学基金资助项目(61603144); 福建省高校产学合作科技重大项目(2013H6016); 福建省自然科学基金资助项目(2018J01095); 华侨大学中青年教师科技创新资助计划项目(ZQN-PY509)
更新日期/Last Update: 2019-07-20