论文部分内容阅读
探讨使用电机式力伺服系统作为一种加载方式,用来仿真飞行器的操纵系统负载力及其变化特性的具体方法。并且介绍了驾驶杆力的数学建模的建立、讨论了电机伺服系统的软件设计和机械接口设计。
This paper discusses how to use the motor servo system as a loading method to simulate the load of the operating system of the aircraft and its changing characteristics. The establishment of mathematical modeling of the driving force is also introduced. The software design and the mechanical interface design of the servo system are discussed.