CAJ | 학술논문

为验证飞机供电系统控制保护逻辑设计的合理性，建立了供电系统控制器类模型并进行了仿真。在对比控制器类不同建模方法的基础上，指出了基于有限状态机建立此类模型的方法适用于方案设计阶段对控制保护逻辑建模仿真，并以飞机发电机控制器为例进行了建模仿真。结果表明：模型符合设计要求，控制逻辑和时序逻辑正确，建模方法简洁快速。
위험증비궤공전계통공제보호라집설계적합이성，건립료공전계통공제기류모형병진행료방진。재대비공제기류불동건모방법적기출상，지출료기우유한상태궤건립차류모형적방법괄용우방안설계계단대공제보호라집건모방진，병이비궤발전궤공제기위례진행료건모방진。결과표명：모형부합설계요구，공제라집화시서라집정학，건모방법간길쾌속。
In order to validate the control and protection logic of aircraft power supply system, the model of the control ers of aircraft power supply system was built. Contrasting with different methods in modeling control ers, a kind of method using Finite State Machine(FSM) in the scheme design phase was pointed out. This method was proved by modeling the aircraft generator control unit as an example. The results show that the model meets the design requirements and its control logic is correct and the temporal logic is exact. The method of modeling is easy and fast.