With the increasing precision of guidance,the impact of autopilot dynamic characteristics and target maneuvering abilities on precision guidance is becoming more and more significant.In order to reduce or even elimina...With the increasing precision of guidance,the impact of autopilot dynamic characteristics and target maneuvering abilities on precision guidance is becoming more and more significant.In order to reduce or even eliminate the autopilot dynamic operation and the target maneuvering influence,this paper suggests a guidance system model involving a novel integral sliding mode guidance law(ISMGL).The method utilizes the dynamic characteristics and the impact angle,combined with a sliding mode surface scheme that includes the desired line-ofsight angle,line-of-sight angular rate,and second-order differential of the angular line-of-sight.At the same time,the evaluation scenario considere the target maneuvering in the system as the external disturbance,and the non-homogeneous disturbance observer estimate the target maneuvering as a compensation of the guidance command.The proposed system’s stability is proven based on the Lyapunov stability criterion.The simulations reveale that ISMGL effectively intercepted large maneuvering targets and present a smaller miss-distance compared with traditional linear sliding mode guidance laws and trajectory shaping guidance laws.Furthermore,ISMGL has a more accurate impact angle and fast convergence speed.展开更多
为解决沙棘叶茶茶毫离散元仿真中缺乏准确接触参数的问题,利用物理和仿真休止角堆积试验标定茶毫接触参数;将茶毫颗粒简化为软质球形颗粒,通过量纲分析和颗粒缩放理论将茶毫空气动力学当量粒径从231.37μm放大至1.8 mm。利用EDEM软件,...为解决沙棘叶茶茶毫离散元仿真中缺乏准确接触参数的问题,利用物理和仿真休止角堆积试验标定茶毫接触参数;将茶毫颗粒简化为软质球形颗粒,通过量纲分析和颗粒缩放理论将茶毫空气动力学当量粒径从231.37μm放大至1.8 mm。利用EDEM软件,选定“Hertz–Mindlin with JKR”接触模型,以休止角为响应值,通过Plackett-Burman试验筛选出对休止角影响最显著的3个参数:茶毫-茶毫恢复系数、茶毫-茶毫滚动摩擦系数、茶毫-不锈钢滚动摩擦系数;利用最陡爬坡试验,确定各参数最佳取值范围;根据Box-Behnken试验建立并优化3个显著性参数与休止角的二阶回归方程,对回归方程进行寻优求解。得到3个显著性参数的最优组合:茶毫-茶毫恢复系数为0.159,茶毫-茶毫滚动摩擦系数为0.290,茶毫-不锈钢滚动摩擦系数为0.239。通过对比休止角仿真试验值与物理试验值,二者相对误差为1.97%,表明仿真试验预测效果良好。展开更多
文摘With the increasing precision of guidance,the impact of autopilot dynamic characteristics and target maneuvering abilities on precision guidance is becoming more and more significant.In order to reduce or even eliminate the autopilot dynamic operation and the target maneuvering influence,this paper suggests a guidance system model involving a novel integral sliding mode guidance law(ISMGL).The method utilizes the dynamic characteristics and the impact angle,combined with a sliding mode surface scheme that includes the desired line-ofsight angle,line-of-sight angular rate,and second-order differential of the angular line-of-sight.At the same time,the evaluation scenario considere the target maneuvering in the system as the external disturbance,and the non-homogeneous disturbance observer estimate the target maneuvering as a compensation of the guidance command.The proposed system’s stability is proven based on the Lyapunov stability criterion.The simulations reveale that ISMGL effectively intercepted large maneuvering targets and present a smaller miss-distance compared with traditional linear sliding mode guidance laws and trajectory shaping guidance laws.Furthermore,ISMGL has a more accurate impact angle and fast convergence speed.
文摘为解决沙棘叶茶茶毫离散元仿真中缺乏准确接触参数的问题,利用物理和仿真休止角堆积试验标定茶毫接触参数;将茶毫颗粒简化为软质球形颗粒,通过量纲分析和颗粒缩放理论将茶毫空气动力学当量粒径从231.37μm放大至1.8 mm。利用EDEM软件,选定“Hertz–Mindlin with JKR”接触模型,以休止角为响应值,通过Plackett-Burman试验筛选出对休止角影响最显著的3个参数:茶毫-茶毫恢复系数、茶毫-茶毫滚动摩擦系数、茶毫-不锈钢滚动摩擦系数;利用最陡爬坡试验,确定各参数最佳取值范围;根据Box-Behnken试验建立并优化3个显著性参数与休止角的二阶回归方程,对回归方程进行寻优求解。得到3个显著性参数的最优组合:茶毫-茶毫恢复系数为0.159,茶毫-茶毫滚动摩擦系数为0.290,茶毫-不锈钢滚动摩擦系数为0.239。通过对比休止角仿真试验值与物理试验值,二者相对误差为1.97%,表明仿真试验预测效果良好。