余度设计

余度设计中的系统可靠性最优分配模型

System Reliability Distribution Optimization Model For Redundancy Design

伺服机构控制信号余度设计研究

Redundancy Design of Servo Mechanism Control Signal

提出了基于BIT的双通道容错电子控制器设计方案，电子控制器包括两个采用相似余度设计的控制通道（A、B通道）和一个监控通道（C通道）。

The design scheme of dual channel fault-tolerant EEC based on BIT was brought forward , which consists of two similar redundant control channels ( channel A and B ) and a monitor channel ( channel C ) .

余度设计是伺服作动系统可靠性设计的重要内容。

Redundant design is an important work of servo-actuation system reliability design .

小型飞行器机载计算机的余度设计技术电传飞行控制系统的余度设计技术

Redundancy Techniques for Fly-By-Wire Flight Control Systems

此外，还分别建立了串并联和并串联两种余度设计系统的最少研制费用模型。

Moreover , the least development cost models for the series-parallel and the parallel-series redundancy design are established .

采用非相似余度设计思想，建立了无人机横侧向控制系统。

With the method of dissimilar redundant design , this paper put forwards a lateral direction control system of UAV .

所给出的余度设计及分布式共享内存策略增强了整个光传系统的可靠性及容错性能。

Redundancy design technology and distributed shared memory strategy were used to enhance the reliability and fault-tolerance capability of the whole system .

控制器采用相似余度设计，给出了硬件电路设计方案和软件程序设计框架，按照功能模块化设计思想分别予以实现。

The controller using similar redundancy has two redundant channels . The hardware circuits and software programs are designed by using modular design of function .

对数控系统的总体结构、控制规律、故障诊断及余度设计、电子控制器、液压机械装置、控制软件开发等关键技术分别进行了讨论。

Key techniques such as system construction , control rules , fault diagnostic approach , electronic controller , hydraulic mechanical unit , and control software are discussed .

飞行控制系统余度方案设计的决策支持系统

DSS of the DFCS 's Redundant Scheme Design

FC环形通信网络双余度容错的设计与实现

Design and Implementation of Dual Redundancy FC Ring Network

不确定系统鲁棒解析余度的最优设计

Optimal Design of Robust Analytical Redundancy for Uncertain Systems

本文介绍了具有混合型三模余度结构的设计与实现。

This paper introduces the design and realization of hybrid structure with three modular redundancy .

一种1553B余度数据总线的设计

Design of a Redundant Data Bus of 1553B

航空发动机双余度智能位置控制器设计

Dual - redundancy smart position controller design for aeroengine

电路设计中实现了系统位置检测、功率驱动、电流采样、电路保护、整流电源、辅助电源及双余度等主要电路设计，给出了速度、电流双闭环控制方法。

Circuit design to achieve a position detection system , power driver and current sampling circuit protection , rectifier power supply , auxiliary power supplies and dual redundant circuit design major given the speed and current dual-closed-loop control method .

介绍了余度技术、容错技术有关概念，概述了它们在飞行控制系统中的应用，并强调了余度管理在余度系统设计中的重要性。

The paper introduces the concepts of redundant and fault-tolerant technique , discusses their application in the flight-control system , and pays more attention to the importance of redundant management in design of the redundant system .