Flight and Vibration Control of Flexible Air-Breathing Hypersonic Vehicles Under Actuator Faults

The issue of modeling and fault-tolerant control (FTC) design for a class of flexible air-breathing hypersonic vehicles (FAHVs) with actuator faults is investigated in this article. Different from previous research, the shear deformation of the fuselage is considered, and an ordinary differential eq...

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Published inIEEE transactions on cybernetics Vol. 53; no. 5; pp. 2741 - 2752
Main Authors He, Xiuyu, Ma, Yonghao, Chen, Mou, He, Wei
Format Journal Article
LanguageEnglish
Published United States IEEE 01.05.2023
The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subjects
Actuators
Adaptation models
Adaptive control
Airframes
Algorithms
Closed loops
Fault tolerance
Fault-tolerant control (FTC)
Faults
Feasibility
Feedback control
flexible air-breathing hypersonic vehicle (FAHV)
Fuselages
Hypersonic vehicles
Liapunov direct method
Linear matrix inequalities
Mathematical analysis
Mathematical models
Partial differential equations
Shear deformation
Stability analysis
Strain
Symmetric matrices
Timoshenko beam (TB)
Vehicle dynamics
Vibration control
vibration suppression
Vibrations
Online AccessGet full text
ISSN2168-2267
2168-2275
2168-2275
DOI10.1109/TCYB.2022.3140536

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Abstract The issue of modeling and fault-tolerant control (FTC) design for a class of flexible air-breathing hypersonic vehicles (FAHVs) with actuator faults is investigated in this article. Different from previous research, the shear deformation of the fuselage is considered, and an ordinary differential equations-partial differential equations (ODEs-PDEs) coupled model is established for the FAHVs. A feedback control is proposed to ensure flight stable and an adaptive FTC method is designed to deal with actuator faults while suppressing the system's vibrations. Besides, the stability analysis of the closed-loop system is given via the Lyapunov direct method and an algorithm that transfers the bilinear matrix inequalities (BMIs) feasibility problem to the linear matrix inequalities (LMIs) feasibility problem is provided for determining the control gains. Finally, the numerical simulation results show that the proposed controller can stabilize the flight states and suppresses the vibration of the fuselage efficiently.
AbstractList The issue of modeling and fault-tolerant control (FTC) design for a class of flexible air-breathing hypersonic vehicles (FAHVs) with actuator faults is investigated in this article. Different from previous research, the shear deformation of the fuselage is considered, and an ordinary differential equations-partial differential equations (ODEs-PDEs) coupled model is established for the FAHVs. A feedback control is proposed to ensure flight stable and an adaptive FTC method is designed to deal with actuator faults while suppressing the system's vibrations. Besides, the stability analysis of the closed-loop system is given via the Lyapunov direct method and an algorithm that transfers the bilinear matrix inequalities (BMIs) feasibility problem to the linear matrix inequalities (LMIs) feasibility problem is provided for determining the control gains. Finally, the numerical simulation results show that the proposed controller can stabilize the flight states and suppresses the vibration of the fuselage efficiently.
The issue of modeling and fault-tolerant control (FTC) design for a class of flexible air-breathing hypersonic vehicles (FAHVs) with actuator faults is investigated in this article. Different from previous research, the shear deformation of the fuselage is considered, and an ordinary differential equations-partial differential equations (ODEs-PDEs) coupled model is established for the FAHVs. A feedback control is proposed to ensure flight stable and an adaptive FTC method is designed to deal with actuator faults while suppressing the system's vibrations. Besides, the stability analysis of the closed-loop system is given via the Lyapunov direct method and an algorithm that transfers the bilinear matrix inequalities (BMIs) feasibility problem to the linear matrix inequalities (LMIs) feasibility problem is provided for determining the control gains. Finally, the numerical simulation results show that the proposed controller can stabilize the flight states and suppresses the vibration of the fuselage efficiently.The issue of modeling and fault-tolerant control (FTC) design for a class of flexible air-breathing hypersonic vehicles (FAHVs) with actuator faults is investigated in this article. Different from previous research, the shear deformation of the fuselage is considered, and an ordinary differential equations-partial differential equations (ODEs-PDEs) coupled model is established for the FAHVs. A feedback control is proposed to ensure flight stable and an adaptive FTC method is designed to deal with actuator faults while suppressing the system's vibrations. Besides, the stability analysis of the closed-loop system is given via the Lyapunov direct method and an algorithm that transfers the bilinear matrix inequalities (BMIs) feasibility problem to the linear matrix inequalities (LMIs) feasibility problem is provided for determining the control gains. Finally, the numerical simulation results show that the proposed controller can stabilize the flight states and suppresses the vibration of the fuselage efficiently.
Author Chen, Mou
He, Xiuyu
He, Wei
Ma, Yonghao
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Snippet The issue of modeling and fault-tolerant control (FTC) design for a class of flexible air-breathing hypersonic vehicles (FAHVs) with actuator faults is...
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SubjectTerms Actuators
Adaptation models
Adaptive control
Airframes
Algorithms
Closed loops
Fault tolerance
Fault-tolerant control (FTC)
Faults
Feasibility
Feedback control
flexible air-breathing hypersonic vehicle (FAHV)
Fuselages
Hypersonic vehicles
Liapunov direct method
Linear matrix inequalities
Mathematical analysis
Mathematical models
Partial differential equations
Shear deformation
Stability analysis
Strain
Symmetric matrices
Timoshenko beam (TB)
Vehicle dynamics
Vibration control
vibration suppression
Vibrations
Title Flight and Vibration Control of Flexible Air-Breathing Hypersonic Vehicles Under Actuator Faults
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