V41 导航通讯系统与设备 标准查询与下载

IEC PAS 62647-1:2011 航空电子设备用流程管理.含无铅焊料的航空航天和防御电子系统.第1部分:无铅管理

Process management for avionics - Aerospace and defence electronic systems containing lead-free solder - Part 1: Lead-free management

IEC PAS 62647-2:2011 航空电子设备用流程管理.含无铅焊料的航空航天和防御电子系统.第2部分:锡的有毒影响的减轻

Process management for avionics - Aerospace and defence electronic systems containing lead-free solder - Part 2: Mitigation of the deleterious effects of tin

BS EN 4660-005:2011 航空航天系列.模块化和开放式航空电子体系结构.软件

The purpose of this European Standard is to establish uniform requirements for design and development of software architecture for modular avionics systems as defined per ASAAC.

Aerospace series. Modular and open avionics architectures. Software

DIN EN 303213-4-2:2011 高级地面移动导航和控制系统(A-SMGCS) 第4部分 包括其接口的非合作传感器部署合作用欧洲单一空中互操作性规则EC 552/2004下应用的共同体规范 第2子部分 部署地面移动雷达传感器的具体要求(英文版本EN 303213-4-2 V1.1.1 (2010-10)作为德国标准)

Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 4: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for a deployed non-cooperative sensor including its interfaces - Sub-pa

DIN EN 303213-3:2011 高级地面移动导航和控制系统(A-SMGCS) 第3部分 包括其接口的传感器部署合作用欧洲单一空中互操作性规则EC 552/2004下应用的共同体规范(英文版本EN 303213-3 V1.1.1 (2010-10)作为德国标准)

Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 3: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for a deployed cooperative sensor including its interfaces (Endorsement

DIN EN 303213-2:2011 高级地面移动导航和控制系统(A-SMGCS).第2部分:A-SMGCS等级2包括外部接口用欧洲单一空中互操作性规则EC 552/2004下应用的共同体规范

Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 2: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for A-SMGCS Level 2 including external interfaces (Endorsement of the E

BS 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.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 in this 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.

Aerospace series. Modular and open avionics architectures. Communications/Network

BS 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.普通功能模块

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 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.

Aerospace series. Modular and open avionics architectures. Common functional modules

BS 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.体系架构

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. Architecture

SAE AS20708/29A-2011 同步控制变压器,型号18CT4C

The requirements for acquiring the Synchros described herein shall consist of this specification and the latest issue of SAE AS 20708.

Synchro, Control Transformer, Type 18CT4C

SAE AS20708/1A-2011 同步控制变压器,型号11CT4E

The requirements for acquiring the Synchros described herein shall consist of this specification and the latest issue of SAE AS 20708.

Synchro, Control Transformer, Type 11CT4E

SAE AS6030-2011 接口标准,公用接口控制计划

This Common Interface Control Plan (CICP) establishes the methodology for developing, controlling and managing the technical interfaces between and within systems. The document is not intended to directly control any other aspects of program management, such as matters of contractual, financial or those of an intellectual property rights nature. Members in the interface control process include: procurement authorities, design authorities and other related agencies as defined in the specific System Interface Control Plan (SICP). For the purposes of this plan only the terms Procuring Organization and Producing Organization will be used. This plan is predicated upon formal agreements between participating organizations that provide: a. Authority to participate in Interface Control Working Group (ICWG) and decision making processes. b. Primary integration control, interface problem resolution, and interface impact assessments through the ICWG. c. Higher level interface management under the purview of the appellate process as defined by this document and in the SICP. The purpose of this CICP is to define the roles, responsibilities, policies, and procedures to be implemented to control the development and refinement of the System Data Set (SDS). This CICP stipulates the policies and procedures required to manage interface control and assure compatibility between system segments/equipment. This plan defines the SDS and its developmental, change, and control requirements. This plan further defines the roles and responsibilities of the ICWG, Interface Management Board (IMB) and any higher levels of the appellate process members (e.g. Interface Control Steering Group (ICSG)). This standard applies to interfaces between and within systems requiring development, control and management. This standard may be applied to existing systems when they are being revised.

Interface Standard, Common Interface Control Plan

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 ISO 12384:2010 航空航天.航空器电源特性测量用数字设备的要求

Aerospace. Requirements for digital equipment for measurements of aircraft electrical power characteristics

ISO 12384:2010 航空航天.飞机电源特性测量用数字设备要求

This International Standard specifies the requirements for digital measuring methods and digital measuring equipment for aircraft electrical power characteristics, including accuracy, algorithms and digital measuring equipment. The measuring equipment should be applied mainly for the use of laboratory or rig tests. This International Standard can be applied to digital measuring equipment which is involved in the measurement of power electrical characteristics of the power supply system, power distributing systems and the utilization of equipment in aircrafts.

Aerospace - Requirements for digital equipment for measurements of aircraft electrical power characteristics

GJB 624.18-2010 军用飞机科研试飞训练要求 第18部分：机载电子对抗

本部分规定了有人驾驶固定翼飞机进行机载电子对抗科研试飞训练的通用要求。 本部分适用于有人驾驶固定翼飞机机载电子对抗科研试飞训练的技术准备、组织实施与评价。特种用途固定翼军用飞机可参照执行。

Training requirements of flight test research for military aircraft.Part 18:Airborne electronic warfare

GJB 7103-2010 无人机测控与信息传输系统消息格式

Message Format of UAV TT&C and Information Transmission System

GJB 7104-2010 无人机测控与信息传输系统信道通用要求

本标准规定了无人机测控与信息传输系统传输信道的相关技术要求。 本标准适用于无人机测控与信息传输系统传输信道设计和制造。

General requirements for wireless channel of UAV tracking telemetry and command (TT&C) communication system

GJB 7105-2010 无人机测控与信息传输系统端机通用要求

本标准规定了无人机测控与信息传输系统端机的功能、性能和接口要求。 本标准适用于无人机测控与信息传输系统端机的设计和制造。

General requirements for terminal of UAV tracking telemetry and command (TT&C)and communication system