单相统一电能质量调节器(single-phase unified power quality conditioner,SPUPQC)是一个强耦合的多输入多输出非线性系统.本文在平衡流形重构系统模型,基于逆系统方法对重构后的系统构造解耦的伪线性系统.针对该伪线性系统采用线性二...单相统一电能质量调节器(single-phase unified power quality conditioner,SPUPQC)是一个强耦合的多输入多输出非线性系统.本文在平衡流形重构系统模型,基于逆系统方法对重构后的系统构造解耦的伪线性系统.针对该伪线性系统采用线性二次型调节器(LQR)设计了满足一定性能指标的控制器.该控制策略有良好的动态响应与补偿效果并有一定的实用价值.仿真实验证明了该控制器设计的可靠性与有效性.展开更多
With the strong battlefield application environment of the next generation fighter,based on the design of distributed vehicle management system,a fault diagnosis and fault-tolerant control(FTC)method for wing surface ...With the strong battlefield application environment of the next generation fighter,based on the design of distributed vehicle management system,a fault diagnosis and fault-tolerant control(FTC)method for wing surface damage is proposed in this paper.Aiming at three kinds of wing damage modes,this paper proposes a diagnosis method based on the fault decision tree and forms a fault decision tree for wing damage from the aspects of sample database construction,feature parameter extraction,and fault decision tree construction.Based on the fault diagnosis results,the longitudinal control law based on dynamic inverse and the lateral-directional robust control laws based on linear quadratic regulator(LQR)are proposed.From the simulation examples,the fault diagnosis algorithm based on the decision tree can complete the judgment of three wing surface damage modes within 2 ms,and the FTC law can make the fighter quickly return to a stable flight state after a short transient of 1 s,which achieves the fault-tolerant goal.展开更多
文摘单相统一电能质量调节器(single-phase unified power quality conditioner,SPUPQC)是一个强耦合的多输入多输出非线性系统.本文在平衡流形重构系统模型,基于逆系统方法对重构后的系统构造解耦的伪线性系统.针对该伪线性系统采用线性二次型调节器(LQR)设计了满足一定性能指标的控制器.该控制策略有良好的动态响应与补偿效果并有一定的实用价值.仿真实验证明了该控制器设计的可靠性与有效性.
基金This work was supported by the Defense Industrial Technology Development Program(JCKY2016205C013).
文摘With the strong battlefield application environment of the next generation fighter,based on the design of distributed vehicle management system,a fault diagnosis and fault-tolerant control(FTC)method for wing surface damage is proposed in this paper.Aiming at three kinds of wing damage modes,this paper proposes a diagnosis method based on the fault decision tree and forms a fault decision tree for wing damage from the aspects of sample database construction,feature parameter extraction,and fault decision tree construction.Based on the fault diagnosis results,the longitudinal control law based on dynamic inverse and the lateral-directional robust control laws based on linear quadratic regulator(LQR)are proposed.From the simulation examples,the fault diagnosis algorithm based on the decision tree can complete the judgment of three wing surface damage modes within 2 ms,and the FTC law can make the fighter quickly return to a stable flight state after a short transient of 1 s,which achieves the fault-tolerant goal.
