对精确时钟同步协议(Procision Time Protocol,PTP)的工作原理、时钟模型、延时测量机制、传输协议栈、通信模式进行了深入分析研究。在协议分析的基础上,结合数字化变电站过程层网络的特点和时间同步要求,分析了PTP1588在数字化变电站...对精确时钟同步协议(Procision Time Protocol,PTP)的工作原理、时钟模型、延时测量机制、传输协议栈、通信模式进行了深入分析研究。在协议分析的基础上,结合数字化变电站过程层网络的特点和时间同步要求,分析了PTP1588在数字化变电站过程层网络应用的关键点。总结了PTP1588协议的应用思路--PTP1588是一个通用的时间同步协议,对于一个特定应用,应根据此特定应用的网络特点和同步指标要求,在PTP1588协议中选取合适的机制和参数来构建此特定应用的PTP1588时间同步方案。展开更多
In this paper, the attitude control algorithm of flexible spacecraft with unknown measurement delay and input delay based on disturbance observer is designed. The influence of measurement delay and input delay on the ...In this paper, the attitude control algorithm of flexible spacecraft with unknown measurement delay and input delay based on disturbance observer is designed. The influence of measurement delay and input delay on the attitude control system and disturbance observer is analyzed. The disturbance estimation error equation is transformed into a differential system with a pure delay. Then, the observer gain is chosen based on the 3/2 stability theorem to ensure the stability and disturbance attenuation performance of the pure delay system. Next, the controller gain is designed based on the Linear Matrix Inequality(LMI) approach to guarantee the stability of the composite system and achieve H_∞ performance with two additive delays. The simulation results show that the proposed method can improve the anti-disturbance ability of the attitude control system.展开更多
文摘对精确时钟同步协议(Procision Time Protocol,PTP)的工作原理、时钟模型、延时测量机制、传输协议栈、通信模式进行了深入分析研究。在协议分析的基础上,结合数字化变电站过程层网络的特点和时间同步要求,分析了PTP1588在数字化变电站过程层网络应用的关键点。总结了PTP1588协议的应用思路--PTP1588是一个通用的时间同步协议,对于一个特定应用,应根据此特定应用的网络特点和同步指标要求,在PTP1588协议中选取合适的机制和参数来构建此特定应用的PTP1588时间同步方案。
基金supported by the National Natural Science Foundation of China (Nos. 61627810, 61320106010, 61633003, 61661136007 and 61603021)the Program for Changjiang Scholars and Innovative Research Team, China (No. IRT_16R03)Innovative Research Team of National Natural Science Foundation of China (No. 61421063)
文摘In this paper, the attitude control algorithm of flexible spacecraft with unknown measurement delay and input delay based on disturbance observer is designed. The influence of measurement delay and input delay on the attitude control system and disturbance observer is analyzed. The disturbance estimation error equation is transformed into a differential system with a pure delay. Then, the observer gain is chosen based on the 3/2 stability theorem to ensure the stability and disturbance attenuation performance of the pure delay system. Next, the controller gain is designed based on the Linear Matrix Inequality(LMI) approach to guarantee the stability of the composite system and achieve H_∞ performance with two additive delays. The simulation results show that the proposed method can improve the anti-disturbance ability of the attitude control system.
