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介绍一种新型结构的可实现飞行器横滚模拟仿真实验的低速单自由度旋转系统,对其整体机械结构和动态性能进行了分析,并结合ADMAS和Simulink进行联合动态仿真。该单自由度旋转系统结构简单,适用性强,可满足多种类型飞行器(包括导弹)等部分分系统产品进行飞行控制测试和半实物仿真的要求。
A new type of low-speed, single-degree-of-freedom rotating system that can achieve aircraft roll simulation is introduced. Its overall mechanical structure and dynamic performance are analyzed. Combined with ADMAS and Simulink, dynamic simulation is carried out. The single-degree-of-freedom rotary system has the advantages of simple structure and strong applicability, and can meet the requirements of flight control testing and semi-physical simulation of a number of subsystems and products of various types of aircraft (including missiles).