据报道,美国空军与多家公司签约执行的飞/推综合控制中的综合控制系统设计方法(DMICS)研究计划中采用LQG/LTR方法,各种先进的多变量控制规律之所以不能在发动机上得到普遍应用的原因是多方面的,其中重要原因之一是:...
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讨论了一种具有飞行与推力综合系统的舰载机自动着舰控制系统的设计方法。
A design method of the automatic control systems with Integrated flight and thrust controls for landing on carrier is discussed in this paper.
本文讨论了如何利用输出反馈配置极点的方法设计大型汽轮发电机组综合控制系统的问题。
The method of -pole assignment for multivariable systems by output feedback and its application to the design of integrated controller of large turbo-generator set are discussed in this paper.
提出了一种基于逆动力学和在线参数辨识的方法,用于直接设计综合控制系统中的姿态控制器。
A synthesis method based on inverse dynamics and online parameter identification was developed and was directly used to design the attitude controller in the integrated control system.
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