1) fault-tolerant aviation control system
容错飞控系统
2) fault-tolerant flight control systems
容错飞行控制系统
3) fault-tolerant control system
容错控制系统
1.
This paper studies a fault-tolerant control system for a space modular manipulator system mounted on space station or other spacecrafts such as satellites, located in low earth orbit.
研究搭载在空间站或其他近地轨道航天器上的空间模块化机械手系统的容错控制系统。
2.
The need of simultaneous stabilization or pole-assignment is due to de-signing fault-tolerant control systems.
同时稳定或极点配置是出于设计容错控制系统之所需。
4) fault-tolerant system
容错系统
1.
In order to solve this problem,a new method for designing BIT fault diagnosis strategy for fault-tolerant systems,considering reliability and testing costs,was proposed based on dynamic fault tree model.
为此,以动态故障树模型为基础,综合考虑可靠性和测试费用等因素,提出了一种面向复杂容错系统的BIT诊断策略设计新方法。
2.
A fault-tolerant system experiences a crash due to hardware components faults or progressive performance degradation as an"aging"phenomenon,because of running continuously for very long periods.
容错系统不仅会产生硬件故障,由于连续长时间的运行,系统的性能也会逐渐下降或失效,即老化现象。
3.
By the example of applying it on the(N+M) fault-tolerant system,analyzes its performance,results show the search efficiency and accuracy of improved particle swarm optimization algorithm are better than general.
通过将其应用于(N+M)容错系统模型的实例,对改进算法的性能进行了分析,结果表明,改进算法的搜索效率和精度均优于一般的粒子群算法,同时具有较好的收敛稳定性。
5) fault tolerant systems
容错系统
1.
In this paper (N+M) fault tolerant systems are studied theoretically.
对（Ｎ＋Ｍ）容错系统进行了初步的理论研究，分析了其可靠性，考察控制器可靠性和维修性对系统可用度的影响，并提出了改善系统可用度的措施。
6) fault tolerant system
容错系统
1.
The basic principle about dynamically re configurable FPGA was introduced and an new design method about the fault tolerant system of digital circuits was presented.
在介绍FPGA动态可重构技术原理的基础上 ,探讨了该技术在数字电路容错系统中的应用方法和构成原理 ,并针对某心脏起搏器电路系统 ,采用FPGA动态可重构方法进行了系统的容错设计与实验 。
2.
N+M) fault tolerant system (FTS) makes full use of the hardware and software of its own, and intelligent networking is a practical way to implement it, so that it is expected to have wide application in control systems.
分析了（Ｎ＋Ｍ）容错系统的经济性，提出了其经济性的优化模型，并利用图视化方法进行了求解，给出了一种简单实用的最佳备件量选取方法。
3.
But it can not be use d to analyze the reliability of fault tolerant systems.
传统的故障树分析 ( Fault Tree Analysis,简称 FTA)方法是一种基于静态逻辑或静态故障机理的方法 ,但这种方法对容错系统的可靠性分析已不适用。
补充资料：飞容
1.飞翔的姿态。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条