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。
When actuator is in trouble, we give a design method of fault tolerant controller for pipeline's normally running.
保证管道运行工况平稳，给出了执行器故障时容错控制器的设计方法。
This paper presents a fault-tolerant software design method and its application to the micro-controller system (MCS-51) of a type of Pilotless aircraft.
本文介绍了某型无人驾驶飞机系列MCS - 51单片机控制系统的软件容错设计方法与实现。
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。
A modified sliding mode fault tolerant controller is developed for flexible spacecraft attitude stabilization control in the presence of loss of actuator effectiveness fault and actuator stuck fault.
针对挠性航天器执行器卡死与失效故障的姿态稳定控制问题，提出了一种结构简单、计算量小的改进型滑模容错控制策略。
The test structure and test method in an air-born real-time fault-tolerant distributed computer system are dealt. The design of test controller and test buses are also discussed briefly.
阐述了机载实时容错分布式计算机系统测试体系结构及测试方法，并简要介绍了测试总线和测试控制器的设计。
The test structure and test method in an air-born real-time fault-tolerant distributed computer system are dealt. The design of test controller and test buses are also discussed briefly.
阐述了机载实时容错分布式计算机系统测试体系结构及测试方法，并简要介绍了测试总线和测试控制器的设计。
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