摘要
介绍了某型航空发动机数字式控制系统的设计。该设计包括系统要求、系统构成和各部件的功能,发动机稳态和过渡态的控制设计方法、开环控制规律和闭环控制规律的转换、PID控制算法各环节系数的优化。
The distal control system design of an aeroengine has been introduced, including the system requirements, configurations and component functions, the transformation of control modes between steady and transient phases and that of the control laws between open- looped and dose- looped states, the optimization of the accommodation coefficients in PID control algorithm and the bench test of this system.
出处
《航空发动机》
2005年第1期10-13,共4页
Aeroengine
