An integral sliding mode guidance law(ISMGL)combined with the advantages of the integral sliding mode control(SMC)method is designed to address maneuvering target interception problems with impact angle constraints.Th...An integral sliding mode guidance law(ISMGL)combined with the advantages of the integral sliding mode control(SMC)method is designed to address maneuvering target interception problems with impact angle constraints.The relative motion equation of the missile and the target considering the impact angle constraint is established in the longitudinal plane,and an integral sliding mode surface is constructed.The proposed guidance law resolves the existence of a steady-state error problem in the traditional SMC.Such a guidance law ensures that the missile hits the target with an ideal impact angle in finite time and the missile is kept highly robust throughout the interception process.By adopting the dynamic surface control method,the ISMGL is designed considering the impact angle constraints and the autopilot dynamic characteristics.According to the Lyapunov stability theorem,all states of the closed-loop system are finally proven to be uniformly bounded.Simulation results are compared with the general sliding mode guidance law and the trajectory shaping guidance law,and the findings verify the effectiveness and superiority of the ISMGL.展开更多
Based on the idea of zeroing the line of sight rate（LOSR）,a novel nonlinear differential geometric（DG） law for intercepting the agile target is proposed.In the first part,the DG formulations are utilized to descri...Based on the idea of zeroing the line of sight rate（LOSR）,a novel nonlinear differential geometric（DG） law for intercepting the agile target is proposed.In the first part,the DG formulations are utilized to describe the relatively kinematics model of missile and target,and the nonlinear DG guidance（DGG） law is proposed based on the nonlinear control theory to eliminate the influence brought by target.Further,the missile guidance commands are derived to overcome the information loss caused by decoupling condition,the new necessary initial condition is developed to guarantee capture the agile target.Then,the designed nonlinear DGG commands are transformed from an arc-length system to the time domain.A desirable aspect of the designed guidance law is that it does not require rigorous information about target acceleration.Representative numerical results show that the designed guidance law obtain a better performance than the traditional DGG law for agile target.展开更多
为降低轮毂电机电动汽车非簧载质量增加对整车操纵稳定性的影响,以某轮毂电机电动汽车电动助力转向系统(Electric Power Steering,EPS)为研究对象,对其参数匹配和控制策略进行研究。设计了目标车型的直线型助力特性曲线,在助力控制的基...为降低轮毂电机电动汽车非簧载质量增加对整车操纵稳定性的影响,以某轮毂电机电动汽车电动助力转向系统(Electric Power Steering,EPS)为研究对象,对其参数匹配和控制策略进行研究。设计了目标车型的直线型助力特性曲线,在助力控制的基础上加入阻尼、回正控制,采用PID控制算法对助力电流进行调节。基于ADAMS/Car搭建轮毂电机电动汽车整车动力学模型,通过MATLAB/Simulink搭建EPS控制模型,实现联合仿真。对操纵稳定性进行了转向盘角阶跃和转向盘角脉冲仿真试验,加入EPS控制后,整车横摆角速度、侧向加速度、质心侧偏角值均有所降低。结果表明:研究的EPS控制策略提高了轮毂电机电动汽车的操纵稳定性,具有较好的控制效果。展开更多
基金supported by the Joint Equipment Fund of the Ministry of Education(6141A02022340)
文摘An integral sliding mode guidance law(ISMGL)combined with the advantages of the integral sliding mode control(SMC)method is designed to address maneuvering target interception problems with impact angle constraints.The relative motion equation of the missile and the target considering the impact angle constraint is established in the longitudinal plane,and an integral sliding mode surface is constructed.The proposed guidance law resolves the existence of a steady-state error problem in the traditional SMC.Such a guidance law ensures that the missile hits the target with an ideal impact angle in finite time and the missile is kept highly robust throughout the interception process.By adopting the dynamic surface control method,the ISMGL is designed considering the impact angle constraints and the autopilot dynamic characteristics.According to the Lyapunov stability theorem,all states of the closed-loop system are finally proven to be uniformly bounded.Simulation results are compared with the general sliding mode guidance law and the trajectory shaping guidance law,and the findings verify the effectiveness and superiority of the ISMGL.
基金supported by the Doctorial Innovation Fund (DY11104)the Aviation Science Innovation Fund of China (20090196005,20100196002)
文摘Based on the idea of zeroing the line of sight rate（LOSR）,a novel nonlinear differential geometric（DG） law for intercepting the agile target is proposed.In the first part,the DG formulations are utilized to describe the relatively kinematics model of missile and target,and the nonlinear DG guidance（DGG） law is proposed based on the nonlinear control theory to eliminate the influence brought by target.Further,the missile guidance commands are derived to overcome the information loss caused by decoupling condition,the new necessary initial condition is developed to guarantee capture the agile target.Then,the designed nonlinear DGG commands are transformed from an arc-length system to the time domain.A desirable aspect of the designed guidance law is that it does not require rigorous information about target acceleration.Representative numerical results show that the designed guidance law obtain a better performance than the traditional DGG law for agile target.
文摘为降低轮毂电机电动汽车非簧载质量增加对整车操纵稳定性的影响,以某轮毂电机电动汽车电动助力转向系统(Electric Power Steering,EPS)为研究对象,对其参数匹配和控制策略进行研究。设计了目标车型的直线型助力特性曲线,在助力控制的基础上加入阻尼、回正控制,采用PID控制算法对助力电流进行调节。基于ADAMS/Car搭建轮毂电机电动汽车整车动力学模型,通过MATLAB/Simulink搭建EPS控制模型,实现联合仿真。对操纵稳定性进行了转向盘角阶跃和转向盘角脉冲仿真试验,加入EPS控制后,整车横摆角速度、侧向加速度、质心侧偏角值均有所降低。结果表明:研究的EPS控制策略提高了轮毂电机电动汽车的操纵稳定性,具有较好的控制效果。
