Results Aero engine linear model within flight envelope designed point and active fault-tolerant controller.
结果得到在飞行包线设计点发动机线性模型和主动容错控制器。
This method can obtain the designed result of fault-tolerant controller by using the linear matrix inequality, and avoids the iterative process of the methods in existence.
该方法利用线性矩阵不等式可方便地得到容错控制器设计结果，避免了现有方法需要重复试验的过程。
A decoupling controller and an approach to the allocation of thruster forces of an AUV are investigated first, then a fault-tolerant control approach under thruster fault is given.
文中先给出在正常情况下水下机器人的解耦控制器及推力分配，然后给出了在推力器出现故障时的容错控制策略。
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