A synchronous control of relative attitude and position is required in separated ultraquiet spacecraft, such as drag-free, disturbance-free, and distributed spacecraft. Thus, a twistorbased synchronous sliding mode co...A synchronous control of relative attitude and position is required in separated ultraquiet spacecraft, such as drag-free, disturbance-free, and distributed spacecraft. Thus, a twistorbased synchronous sliding mode control is investigated in this paper to solve the control problem of relative attitude and position among separated spacecraft modules. The twistor-based control design and the stability proof are implemented using the Modified Rodrigues Parameter（MRP）.To evaluate the effectiveness of the proposed control method, this paper presents a case study of separated spacecraft flying control considering the mass uncertainty and external disturbances. In addition, a simulation study of the Proportional-Derivative（PD） control is also presented for comparison. The results indicate that the twistor-based sliding mode controller can ensure global asymptotic stability. The states converge fast with ultra-precision and ultra-stability in both the attitude and position. Moreover, the proposed twistor-based sliding mode control system is robust to the mass uncertainty and external disturbances.展开更多
针对无位置传感器内置式永磁同步电机(IPMSM)初始位置检测中,传统的基于凸极跟踪的短脉冲电压注入法难以确定脉冲宽度和幅值、实现困难、二次谐波分量法信噪比低的缺点,提出一种基于无滤波器方波信号注入的IPMSM初始位置检测方法。首先...针对无位置传感器内置式永磁同步电机(IPMSM)初始位置检测中,传统的基于凸极跟踪的短脉冲电压注入法难以确定脉冲宽度和幅值、实现困难、二次谐波分量法信噪比低的缺点,提出一种基于无滤波器方波信号注入的IPMSM初始位置检测方法。首先通过向观测的转子d轴注入高频方波电压信号,采用无滤波器载波信号分离方法解耦位置误差信息,通过位置跟踪器获取磁极位置初定值;然后基于磁饱和效应,通过施加方向相反的d轴电流偏置给定,比较d轴高频电流响应幅值大小实现磁极极性辨识;最后,通过2.2k W IPMSM矢量控制系统对提出的基于无滤波器方波信号注入的初始位置检测方法进行实验验证。结果表明,所提方法收敛速度较快,可在IPMSM转子静止或自由运行状态实现初始位置辨识和低速可靠运行,位置观测误差最大值为6.9°。展开更多
基金supported by the National Natural Science Foundation of China(Nos.51675430,11402044,and U1537213)
文摘A synchronous control of relative attitude and position is required in separated ultraquiet spacecraft, such as drag-free, disturbance-free, and distributed spacecraft. Thus, a twistorbased synchronous sliding mode control is investigated in this paper to solve the control problem of relative attitude and position among separated spacecraft modules. The twistor-based control design and the stability proof are implemented using the Modified Rodrigues Parameter（MRP）.To evaluate the effectiveness of the proposed control method, this paper presents a case study of separated spacecraft flying control considering the mass uncertainty and external disturbances. In addition, a simulation study of the Proportional-Derivative（PD） control is also presented for comparison. The results indicate that the twistor-based sliding mode controller can ensure global asymptotic stability. The states converge fast with ultra-precision and ultra-stability in both the attitude and position. Moreover, the proposed twistor-based sliding mode control system is robust to the mass uncertainty and external disturbances.
文摘针对无位置传感器内置式永磁同步电机(IPMSM)初始位置检测中,传统的基于凸极跟踪的短脉冲电压注入法难以确定脉冲宽度和幅值、实现困难、二次谐波分量法信噪比低的缺点,提出一种基于无滤波器方波信号注入的IPMSM初始位置检测方法。首先通过向观测的转子d轴注入高频方波电压信号,采用无滤波器载波信号分离方法解耦位置误差信息,通过位置跟踪器获取磁极位置初定值;然后基于磁饱和效应,通过施加方向相反的d轴电流偏置给定,比较d轴高频电流响应幅值大小实现磁极极性辨识;最后,通过2.2k W IPMSM矢量控制系统对提出的基于无滤波器方波信号注入的初始位置检测方法进行实验验证。结果表明,所提方法收敛速度较快,可在IPMSM转子静止或自由运行状态实现初始位置辨识和低速可靠运行,位置观测误差最大值为6.9°。
