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Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults
被引量:
9
1
作者
Fengying Zheng
Ziyang Zhen
huajun gong
《Journal of Systems Engineering and Electronics》
SCIE
EI
CSCD
2017年第2期322-337,共16页
The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output...
The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output state observer, adaptive fuzzy control, and constraint backstepping technology, a robust fault tolerant control approach is proposed. An output state observer with fuzzy logic systems is developed to estimate unmeasured states, and command filters rather than differentiations of virtual control law are used to solve the computational complexity problem in traditional backstepping. Additionally, a robust term is introduced to offset the fuzzy adaptive estimation error and external disturbance, and an appropriate fault controller structure with matching conditions obtained from fault compensation is proposed. Based on the Lyapunov theory, the designed control program is illustrated to guarantee that all the closed-loop signals of the given system are bounded, and the output errors converge to a small neighborhood of zero. A carrier-based UAV nonlinear longitudinal model is employed to testify the feasibility and validity of the control scheme. The simulation results show that all the controllers can perform at a satisfactory level of reference tracking despite the existence of unknown aerodynamic parameters and actuator faults. © 2017 Beijing Institute of Aerospace Information.
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关键词
Actuators
Aircraft
control
BACKSTEPPING
Control
system
analysis
Control
theory
Controllers
Error
compensation
Fault
tolerance
Flight
control
systems
Fuzzy
control
Fuzzy
filters
Fuzzy
logic
State
estimation
Three
term
control
systems
Unmanned
aerial
vehicles
(UAV)
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题名
Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults
被引量:
9
1
作者
Fengying Zheng
Ziyang Zhen
huajun gong
机构
College of Astronautics
College of Automation Engineering
出处
《Journal of Systems Engineering and Electronics》
SCIE
EI
CSCD
2017年第2期322-337,共16页
基金
supported by the National Nature Science Foundation of China(61304223)
the Aeronautical Science Foundation of China(2016ZA52009)
the Research Fund for the Doctoral Program of Higher Education of China(20123218120015)
文摘
The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output state observer, adaptive fuzzy control, and constraint backstepping technology, a robust fault tolerant control approach is proposed. An output state observer with fuzzy logic systems is developed to estimate unmeasured states, and command filters rather than differentiations of virtual control law are used to solve the computational complexity problem in traditional backstepping. Additionally, a robust term is introduced to offset the fuzzy adaptive estimation error and external disturbance, and an appropriate fault controller structure with matching conditions obtained from fault compensation is proposed. Based on the Lyapunov theory, the designed control program is illustrated to guarantee that all the closed-loop signals of the given system are bounded, and the output errors converge to a small neighborhood of zero. A carrier-based UAV nonlinear longitudinal model is employed to testify the feasibility and validity of the control scheme. The simulation results show that all the controllers can perform at a satisfactory level of reference tracking despite the existence of unknown aerodynamic parameters and actuator faults. © 2017 Beijing Institute of Aerospace Information.
关键词
Actuators
Aircraft
control
BACKSTEPPING
Control
system
analysis
Control
theory
Controllers
Error
compensation
Fault
tolerance
Flight
control
systems
Fuzzy
control
Fuzzy
filters
Fuzzy
logic
State
estimation
Three
term
control
systems
Unmanned
aerial
vehicles
(UAV)
Keywords
Actuators
Aircraft control
Backstepping
Control system analysis
Control theory
Controllers
Error compensation
Fault tolerance
Flight control systems
Fuzzy control
Fuzzy filters
Fuzzy logic
State estimation
Three term control systems
Unmanned aerial vehicles (UAV)
分类号
E926.392 [兵器科学与技术—武器系统与运用工程]
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作者
出处
发文年
被引量
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1
Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults
Fengying Zheng
Ziyang Zhen
huajun gong
《Journal of Systems Engineering and Electronics》
SCIE
EI
CSCD
2017
9
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