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。
Results Aero engine linear model within flight envelope designed point and active fault-tolerant controller.
被动容错控制和主动容错控制多依赖于系统的模型：定量，半定量或定性模型。
Generally, passive and active fault tolerant control systems depend on system models-quantitative, qualitative or quasi - quantitative.
关于广义系统的主动容错控制，研究了基于状态观测器的线性广义系统的主动容错控制的问题。
On the active fault-tolerant control for descriptor systems, the problem of observer-based active fault-tolerant control for descriptor linear systems is considered.
为了验证所提出的主动容错策略的有效性，针对两级倒立摆系统中的电机测速回路故障问题，设计了主动容错控制器。
To demonstrate the effectiveness of the proposed method, an active fault tolerant controller is designed for a double inverted pendulum system with a fault in the motor tachometer loop.
为了验证所提出的主动容错策略的有效性，针对两级倒立摆系统中的电机测速回路故障问题，设计了主动容错控制器。
To demonstrate the effectiveness of the proposed method, an active fault tolerant controller is designed for a double inverted pendulum system with a fault in the motor tachometer loop.
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