Fault tolerant control design for hypersonic UAV attitude dynamical systems with actuator faults

被引：0

作者：

Gao, Zhifeng ^{[1
]}

Qian, Moshu ^{[2
]}

Yin, Jun ^{[3
]}

Lin, Jinxing ^{[1
]}

He, Haikuo ^{[4
]}

机构：

[1] College of Automation, Nanjing University of Posts and Telecommunications, No. 9, Wenyuan Road, Yadongxincheng District, Nanjing 210046, China

[2] Institute of UAV, Nanjing University of Aeronautics and Astronautics, No. 29, Yudao Street, Baixia District, Nanjing 210016, China

[3] College of Information Science and Technology, Donghua University, No. 2999, Renmin North Road, Songjiang District, Shanghai 201620, China

[4] Department of Computer and Information Engineering, Chengde Petroleum College, Chengde 067000, China

来源：

ICIC Express Letters, Part B: Applications | 2012年 / 3卷 / 05期

关键词：

Aircraft detection - Antennas - Dynamical systems - Fault tolerance - Aircraft control - Hypersonic aerodynamics - Backstepping - Actuators - Bandpass filters - Hypersonic vehicles - Adaptive control systems;

D O I：

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中图分类号：

学科分类号：

摘要：

引用

页码：1293 / 1301