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为了掌握自动飞行器的工作特性,在它飞上空中之前,工程技术人员要在地面进行各种仿真试验。研制力矩控制系统的目的在于模拟随高度、速度变化且连续作用在飞行器翼面上的气动铰链力矩。这种装置广泛应用于各种型号舵机。 我们研制的力矩控制系统力案如图1所示。
In order to grasp the working characteristics of an aircraft, engineers must perform various simulation tests on the ground before it can fly into the air. The purpose of developing a torque control system is to simulate the moment of the aerodynamic hinge acting on the airfoil of the aircraft as a function of altitude and velocity. This device is widely used in various types of steering gear. We developed a torque control system case shown in Figure 1.