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感应同步器测角装置目前已广泛地用在宇宙航行、航空设备、军事工业、机械制造、天文观测等国防科研及国民经济建设事业中,日益显著地发挥着它的积极作用。本文提供了一个高速跟踪脉冲调宽型感应同步器测角装置的数学模型,求出了系统的状态方程及其通解公式,又在此基础上推导了该继电系统的时间最优控制的转换方程,为正确设计系统提供了一些理论依据。
Induction synchronizer angle measuring device has been widely used in the aerospace navigation, aviation equipment, military industry, machinery manufacturing, astronomical observation and other national defense scientific research and national economic construction, the increasingly significant play its positive role. In this paper, a mathematical model of the angle measuring device of high speed tracking pulse-width-modulated induction synchronizer is provided. The state equation of the system and its general solution are obtained. Based on this, the transition of time-optimal control of the relay system is deduced The equations provide some theoretical basis for the correct design of the system.