采用全权限数字式电子控制技术是航空发动机控制的一种发展趋势，电子控制器是控制系统中最核心的部分。
The technology of full authority digital electronic control is a trend of aeroengine control, and the electronic controller is the primary part in an aeroengine control system.
本文从数学模型和控制器两方面着手研究提高航空发动机控制系统自适应性的方法。
To improve the adaptive capability of aeroengine control system, the research on mathematic model and controller has been conducted in present thesis.
实验结果表明该智能位置控制器适用于航空发动机分布式控制系统。
The result indicates that the smart position actuator can be applied to aeroengine distributed control systems.
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