49.090 机上设备和仪器 标准查询与下载

DS/EN 4660-002:2011 航空航天系列-模块化和开放式航空电子体系结构-第002部分：通用功能模块

This standard defines the functionality and principle interfaces for the Common Functional Module (CFM) to ensure the interoperability of Common Functional Modules and provides design guidelines to assist in implementation of such a CFM. It is one of a set of standards that define an ASAAC (Allied Standard Avionics Architecture Council) Integrated Modular Avionics System. This definition of interfaces and functionality allows a CFM design that is interoperable with all other CFM to this standard, that is technology transparent, that is open to a multi-vendor market and that can make the best use of COTS technologies. Although the physical organisation and i

Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules

DS/EN 4660-003:2011 航空航天系列 模块化和开放式航空电子体系结构 第003部分：通信/网络

This standard details the functionality and principle interfaces for the ASAAC (Allied Standard Avionics Architecture Council) Network to ensure the interoperability of Common Functional Modules and design guidelines to assist in implementation of such a network. It is one of a set of standards that define an ASAAC Integrated Modular Avionics (IMA) System. The purpose of this standard is to establish by means of well defined interfaces and functionality, a network design that is technology transparent, that is open to a multi-vendor market and that can make the best use of Commercial Off The Shelf (COTS) technologies. Therefore, the associated data communic

Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network

DS/EN 4660-001:2011 航空航天系列 模块化和开放式航空电子体系结构 第001部分：体系结构

The purpose of this standard is to establish uniform requirements for the architecture for Integrated Modular Avionic (IMA) systems as defined by the ASAAC Programme.The IMA architecture can be built by using common components. These components are specified in separate standards. Ways of using these components are described in a set of guidelines. This document gives references to these Standards and Guidelines as well as a short introduction to IMA.

Aerospace series - Modular and Open Avionics Architectures - Part 001: Architecture

DIN EN 4641-103:2011 航空和航天系列.外径为125 m的包层光缆.第103部分:标称外径为2,74 mm的半松包强化单绞芯结构62,5/125mm GI光纤.产品标准;德文版本和英文版本EN 4641-103-2010

Aerospace series - Cables, optical 125 m diameter cladding - Part 103: Semi-loose, ruggedized simplex construction 62,5/125 m GI fibre nominal 2,74 mm, outside diameter - Product standard; German and English version EN 4641-103:2010

LST EN 4641-103-2011 航空航天系列 光缆，直径 125 µm 包层 第103部分：半松散、坚固的单工结构 62,5/125 µm GI 光纤标称 2,74 mm，外径 产品标准

Aerospace series - Cables, optical 125 ?m diameter cladding - Part 103: Semi-loose, ruggedized simplex construction 62,5/125 ?m GI fibre nominal 2,74 mm, outside diameter - Product standard

LST EN 4641-105-2011 航空航天系列 光缆，直径 125 μm 包层 第105部分：半松散、加固四轴结构 62,5/125 μm GI 光纤标称，5,72 mm 外径 产品标准

Aerospace series - Cables, optical 125 ?m diameter cladding - Part 105: Semi-loose, ruggedized quadraxial construction 62,5/125 µm GI fibre nominal, 5,72 mm outside diameter - Product standard

SAE AS6003-2011 TTP通信协议

This SAE Aerospace Standards (AS) establishes the specification for TTP communication protocol functionality as a core networking component for design of synchronous, time-triggered distributed real-time communication networks. This document is referred to as the "base" specification, containing the generic specification of TTP communication protocol functionality, and frame formats, communication services and protocol state machines with transitions, TTP node operation, TTP network operation, distributed clock synchronization and error detection on the network layer. The details described in this standard enable interoperable TTP controller implementations.

TTP Communication Protocol

EN 4660-004:2011 航空航天系列.模块化和开放的航空电子设备的架构.第004部分:包装

The purpose of this standard is to establish uniform requirements for Packaging for the Common Functional Modules (CFM) within an Integrated Modular Avionic (IMA) system, as defined per ASAAC. It comprises the module physical properties and the Module Physical Interface (MPI) definitions together with guidelines for IMA rack and the operational environment. The characteristics addressed by the Packaging Standard are: Interchangeability:-For a given cooling method all modules conforming to the packaging standard will function correctly when inserted into any rack slot conforming to the standard for the cooling method.-All modules conforming to the Module Physical Interface (MPI) definitions for connector, IED and cooling interface will function correctly when inserted into any rack slot conforming to the same MPI definition.; Maintainability:-All modules are easily removable at first line.-No special tools required at first line.-No manual adjustment is necessary when installing modules. No tool is required for installation or removal of the modules.-Mechanical keying is provided that prevents insertion of a module into a rack slot that may cause an unsafe condition.; The Module Physical Interface definition, contained withinThis standard, does not include the properties of the signalling used in the optical interface (e. g. wavelength). These are covered in EN 4660-003.

Aerospace series - Modular and Open Avionics Architectures - Part 004: Packaging

EN 4660-001:2011 航空航天系列.模块化和开放式航空电子系统结构.第001部分:结构

The purpose of this standard is to establish uniform requirements for the architecture for Integrated Modular Avionic (IMA) systems as defined by the ASAAC Programme. The IMA architecture can be built by using common components. These components are specified in separate standards. Ways of using these components are described in a set of guidelines.This document gives references to these Standards and Guidelines as well as a short introduction to IMA.

Aerospace series - Modular and Open Avionics Architectures - Part 001: Architecture

EN 4660-003:2011 航空航天系列.模块化和开放的航空电子设备的架构.第003部分:通信,网络

This standard details the functionality and principle interfaces for the ASAAC (Allied Standard Avionics Architecture Council) Network to ensure the interoperability of Common Functional Modules and design guidelines to assist in implementation of such a network. It is one of a set of standards that define an ASAAC Integrated Modular Avionics (IMA) System. The purpose of this standard is to establish by means of well defined interfaces and functionality, a network design that is technology transparent, that is open to a multi-vendor market and that can make the best use of Commercial Off The Shelf (COTS) technologies. Therefore, the associated data communication network topology, protocols and technologies are not identified inThis document. For these items the document identifies the issues that should be considered when defining a specific network implementation to support the ASAAC architecture and provides guidelines to assist. Although the physical organisation and implementation of the network shall remain the System Designers choice, in accordance with the best use of the current technology, it is necessary to define interfaces and parameter sets in order to achieve a logical definition of the network with a defined functionality.This definition includes:-The generic functionality applicable to all networks.;-The logical interfaces to the Operating System and Module Support Layers.;-The physical interfaces to the Common Functional Modules (CFM). The ASAAC Standards are intended to be independent of specific technologies, including network technologies.This document identifies the principle interfaces for the Network, in Clause 4, and where appropriate, provides requirements on network parameters to be defined. The interfaces relevant to the network are the Module Support Layer to Operating System (MOS), Module Physical Interface (MPI) and Module Logical Interface (MLI). The MOS and MPI are generically defined elsewhere (Standards for Software see EN 4660-005 and Packaging see EN 4660-004). The MLI is clearly a function of the selected network. The MOS and MPI definitions are generic and will need to be supported by network specific information. There is no network-dependent information in the Software or Packaging standards. So a future network specification will not only define the particular MLI, but will also need to define the specific aspects of the MPI, topologies, system properties etc. The definition of the complete Communications and Network Interfaces is partitioned and is covered by the following ASAAC standards:-Network physical Interfaces-ASAAC Standards for Packaging;-Module to Module Communication functions-ASAAC Standards for Software;-Operating System to Network interface-ASAAC Standards for Software;-CFM Software Architecture-ASAAC Standards for Software;-Network physical requirements and properties that define the capability and behaviour required to support CFM to CFM communications-This document.

Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network

EN 4660-002:2011 航空航天系列.模块化和开放的航空电子设备的架构.第002部分:常见的功能模块

This standard defines the functionality and principle interfaces for the Common Functional Module (CFM) to ensure the interoperability of Common Functional Modules and provides design guidelines to assist in implementation of such a CFM. It is one of a set of standards that define an ASAAC (Allied Standard Avionics Architecture Council) Integrated Modular Avionics System.This definition of interfaces and functionality allows a CFM design that is interoperable with all other CFM toThis standard, that is technology transparent, that is open to a multi-vendor market and that can make the best use of COTS technologies. Although the physical organisation and implementation of a CFM should remain the manufacturer's choice, in accordance with the best use of the current technology, it is necessary to define a structure for each CFM in order to achieve a logical definition of the CFM with a defined functionality.This definition includes:-The Generic CFM, which defines the generic functionality applicable to the complete set of CFMs. The generic functionality is defined in 4.1.-The processing capability, which defines the unique functionality associated with each CFM type within the set.This functionality is defined in 4.3.-The logical and physical interfaces that enable CFMs to be interoperable and interchangeable, these are defined in Clause 6.-The functionality required by a CFM to support the operation of the System is defined in Clause 6.; The definition of the complete CFM is partitioned and is covered by the following ASAAC standards:-CFM Mechanical properties and physical Interfaces-ASAAC Standards for Packaging;-CFM Communication functions-ASAAC Standards for Software;-CFM Network interface-ASAAC Standards for Communications and Network;-CFM Software architecture-ASAAC Standards for Software;-CFM Functional requirements-This document.

Aerospace series - Modular and Open Avionics Architectures - Part 002: Common Functional Modules

IEC 107/146/CD:2011 IEC/TS 62668-1:航空电子设备的过程管理.仿造保护.第1部分:避免使用仿造,欺诈和回收的电子元器件组件的指南

IEC/TS 62668-1: Process management for avionics - Counterfeiting protection - Part 1: Guidelines for avoiding the use of counterfeited, fraudulent and recycled electronic components

IEC 107/145/CD:2011 IEC/TS 62239-1:航空电子设备的过程管理.管理计划.第1部分:电子元器件管理计划的准备和维护

IEC/TS 62239-1: Process management for avionics - Management plan - Part 1: Preparation and maintenance of an electronic components management plan

BS EN 4641-105:2010 航空航天系列.包层直径为125微米的光缆.半松强化四层结构62.5/125微米GI纤维,外部标称直径为5.72 mm.产品标准

Aerospace series. Cables, optical 125 $Gmm diameter cladding. Semi-loose, ruggedized quadraxial construction 62,5/125 $Gmm GI fibre nominal, 5,72 mm outside diameter. Product standard

BS EN 4641-103:2010 航空航天系列.电缆,25 $Gmm光学直径包层.半松散,加固单结构62,5/125 $Gmm GI 纤维公称外径2,74 mm.产品标准

Aerospace series. Cables, optical 125 $Gmm diameter cladding. Semi-loose, ruggedized simplex construction 62,5/125 $Gmm GI fibre nominal 2,74 mm, outside diameter. Product standard

BS EN 4641-104:2010 航空航天系列.125 $Gmm径的覆层光缆.半松散强化双重结构标称62,5/125 $Gmm,外径4,95 mm的玻璃纤维.产品标准

Aerospace series. Cables, optical 125 $Gmm diameter cladding. Semi-loose, ruggedized duplex construction 62,5/125 $Gmm GI fibre nominal, 4,95 mm outside diameter. Product standard

SAE AS6040-2010 无人系统联合体系结构(JAUS)人机界面(HMI)设施装置

This document defines a set of standard application layer interfaces called JAUS HMI Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned systems to communicate and coordinate their activities. The HMI Services represent the platform-independent Human Machine Interface (HMI) capabilities commonly found across all domains and types of unmanned systems. Five services are defined in this document: Drawing; Pointing Device; Keyboard; Digital Control; Analog Control Each service is described by a JAUS Service Definition (JSD) which specifies the message set and protocol required for compliance. Each JSD is fully compliant with the JAUS Service Interface Definition Language (JSIDL) (AS5684). The purpose of this document is to provide unmanned systems, subsystems, and payloads a standard message set for the definition of HMI drawing functions and associated control mechanisms. While this standard does not mandate a particular application, a common use allow an unmanned system to provide a consistent user interface across a variety of Operator Control Units (OCUs).

JAUS HMI Service Set

SAE AS6060-2010 无人系统联合体系结构(JAUS)环境感应式耐用装置

This document defines a set of standard application layer interfaces called JAUS Environment Sensing Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned systems to communicate and coordinate their activities. The Environment Sensing Services represent typical environment sensing capabilities commonly found across all domains and types of unmanned systems in a platform-independent manner. At present, five services are defined in this document: Range Sensor: Determine the proximity of objects in the platform's environment Visual Sensor: Provides common configuration and setup for different types of imaging systems Digital Video: A type of Visual Sensor that manages digital video Analog Video: A type of Visual Sensor that manages analog video Still Image: A type of Visual Sensor that manages and encodes individual digital images Each service is described by a JAUS Service Definition (JSD) which specifies the message set and protocol required for compliance. Each JSD is fully compliant with the JAUS Service Interface Definition Language (AS5684). The purpose of this document is to facilitate interoperation of unmanned vehicle systems, subsystems, and payloads by standardization of the message set and associated protocol.

JAUS Environment Sensing Service Set

DIN EN 4645-004:2010 航空航天系列.光学圆型单芯和多芯连接头,螺纹环耦合,自锁定式1.25 mm直径金属包头,带可移动校准套筒支架的连接器.第004部分:安全螺母插座.德文和英文版本EN 4645-004-2009

Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 004: Jam nut receptacle - Product standard; German and English version EN

DIN EN 4645-005:2010 航空航天系列.光学圆型单芯和多芯连接头,螺纹环耦合,自锁定式1.25 mm直径金属包头,带可移动校准套筒支架的连接器.第005部分:插头.产品标准.德文和英文版本EN 4645-005-2009

Aerospace series - Connectors, optical, circular, single and multipin, coupled by threaded ring, self-locking 1,25 mm diameter ferrule with removable alignment sleeve holder - Part 005: Plug - Product standard; German and English version EN 4645-005:2009