Adaptive inverse control structure for nonlinear systems is applied for aeroengine control systems.
研究了航空发动机的非线性自适应逆控制方案。
The augmented LQL method was proposed, then the aeroengine control system was designed by using the method.
并提出了增广l QL控制方法，应用其设计了航空发动机控制系统。
All experiments have showed that the design meets the requirements of distributed aeroengine control system.
实验表明设计的通信方案可以满足航空发动机分布式控制系统要求。
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