V07 电子计算机应用 标准查询与下载

QJ 2543A-2008 航天型号软件维护

Aerospace model software maintenance

BS EN ISO 19134:2008 地理信息.基于位置导航服务.多模型路径与导航

This International Standard specifies the data types and their associated operations for the implementation of multimodal location-based services for routing and navigation. It is designed to specify web services that may be made available to wireless devices through web-resident proxy applications, but is not limited to that environment.

Geographic information - Location-based services - Multimodal routing and navigation

BS EN ISO 19132:2008 地理信息.基于位置导航服务.参考模型

This International Standard defines a reference model and a conceptual framework for location-based services (LBS), and describes the basic principles by which LBS applications may interoperate. This framework references or contains an ontology, a taxonomy, a set of design patterns and a core set of LBS service abstract specifications in UML. This International Standard further specifies the framework's relationship to other frameworks, applications and services for geographic information and to client applications. This International Standard addresses, for an LBS system, the first three basic viewpoints as defined in the Reference Model for Open Distributed Processing (RM-ODP, see ISO/IEC 10746-1). These viewpoints are the a) Enterprise Viewpoint – detailing the purpose, scope, and policies of the system, b) Information Viewpoint – detailing the semantics of information and processing within the system, c) Computational Viewpoint – detailing the functional decomposition of the system. The fourth and fifth viewpoints are addressed only in requirements or examples. These are the d) Engineering Viewpoint – detailing the infrastructure for distribution, e) Technology Viewpoint – detailing the technology for implementation. Reference models and frameworks can be defined at a variety of levels, from conceptual design to software documentation. This International Standard - defines the conceptual framework for, and the type of applications included within, LBS, - establishes general principles for LBS for both mobile and fixed clients, - specifies the interface for data access while roaming, - defines the architectural relationship with other ISO geographic information standards, - identifies areas in which further standards for LBS are required. This International Standard does not address the following issues: - rules by which LBS are developed; - general principles for roaming agreements for mobile clients and tracking targets.

Geographic information. Location based services. Reference model

GJB 6291-2008 导弹部队指挥自动化系统与专用系统接口要求

本标准规定了导弹部队指挥自动化系统与核爆炸探测、武器监控、战训遥测、导弹弹道测量、安全警戒等专用系统之间的接口要求。 本标准适用于导弹部队指挥自动化系统与专用系统连接接口的综合论证、研制、使用和管理。

Interface requirements for missile army command automated system and dedicated system

GJB 6292-2008 指挥自动化设备互换性通用要求

本标准规定了指挥自动化的系统论证、研制和使用等各阶段同类设备的互换性基本要求 本标准适用于军队指挥自动化系统战术技术指标论证及全寿命周期内与设备互换性有关的研制、使用和维护。

General requirements for command automated equipments interchangeability

HB 7836-2008 航空工业电子公文文档一体化管理要求

本标准规定了航空工业电子公文文档一体化管理的一般原则、过程和元数据要求。 本标准适用于航空工业电子公文及其档案的管理。

Integration management requirements of aviation industry electronic offlcial documents and archives

HB/Z 360-2008 航空电子应用软件接口应用指南

本指导性技术文件规定了航空电子系统中应用软件与嵌入式实时操作系统之间接口的应用指南，主要包括功能指南和接口指南。 本指导性技术文件适用于航空电子系统软件产品的开发，包括机载设备和地面支持设备中的软件、独立的软件产品和用于产品验证和确认的软件。

Application guidance for avionics application software interface

GJB 6198-2008 空-空导弹用线加速度计通用规范

本规范规定了空-空导弹用线加速度计的要求、质量保证规定及交货准备等。 本规范适用于空-空导弹用线加速度计（以下简称为加速度计）设计、制造、检验和交付。其他形式的加速度计亦可参照使用。

General specification for air-air missile line accelerometer

GJB 2185A-2008 飞机外部电源监控器通用规范

本规范规定了飞机外部电源监控器（以下简称监控器）的通用技术要求、质量保证规定、交货准备等。 本规范适用于军用飞机上安装的115V、400Hz交流或28V直流监控器。其他监控器可参照使用。

General specification for external electrical power monitors of aircraft

HB 7837-2008 航空产品数字化文件档案管理通用要求

本标准规定了航空产品数字化设计制造中文件的形成、归档、发放和数字化档案的利用、备份、保管、迁移、鉴定、统计等工作的要求。 本标准适用于航空产品数字化文件、数字化档案的管理。

General requirements for digitized document and archive management of aeronautic products

BS ISO 17355:2007 空间数据和信息传输系统.空间数据系统咨询委员会(CCSDS)文档传送协议

This International Standard defines a CCSDS file delivery protocol (CFDP) and associated service for application in the space environment. It is intended for use over the current and envisaged packet delivery services used in the space environment, including ⎯ CCSDS conventional packet telecommand; ⎯ CCSDS conventional packet telemetry; ⎯ CCSDS advanced orbiting systems (AOS) path service. It may also operate over a wide variety of ground network services, including those specified by the CCSDS for cross-support purposes. The protocol operates in the space-to-ground, ground-to-space, and space-tospace directions of transfer. It may be initiated by the file sending or receiving entity. In the interests of interoperability, protocol elements are included for generalized forms of standard file manipulation operations based on assumptions of a common model for a ‘filestore’, or medium used to store files. It is recognized, however, that the precise nature and capabilities of filestore management systems are operating-system dependent and, for that reason, the protocol assumes a virtual filestore and associated services that an implementation must map to the capabilities of the actual filestore used. The scope and field of application are furthermore detailed in subclauses 1.2 and 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - CCSDS file delivery protocol

ISO 22663:2007 航天数据和信息传输系统.接近1的空间链接协议.数据链路层

This International Standard defines the Proximity-1 space link protocol data link layer (framing, media access, data services, and input-output sublayers). It specifies the protocol data units, framing, media access control, expedited and sequenced controlled data transfer, timing service, i/o control, as well as the procedures for establishing and terminating a session between a caller and responder. The coding and synchronization sublayer is defined in ISO 21459. The physical layer is defined in ISO 21460. This International Standard does not specify a) individual implementations or products; b) implementation of service interfaces within real systems; c) the methods or technologies required to perform the procedures; or d) the management activities required to configure and control the protocol. The scope and field of application are furthermore detailed in subclause 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - Proximity-1 space link protocol - Data link layer

ISO 22642:2005/cor 1:2007 航天数据和信息传输系统.TC(遥测指令)同步和信道编码.技术勘误1

This standard is Space data and information transfer systems — TC (telecommand) synchronization and channel coding TECHNICAL CORRIGENDUM 1

Space data and information transfer systems - TC (telecommand) synchronization and channel coding; Technical Corrigendum 1

ISO 22666:2007 航天数据和信息传输系统.AOS(高级轨道系统)航天数据连接协议

This International Standard specifies the advanced orbiting systems (AOS) space data link protocol, a data link layer protocol as defined in ISO/IEC 7498-1, that is to be used over space-to-ground, ground-to-space, or space-to-space communications links by space missions. The scope and field of application are furthermore detailed in subclauses 1.2 and 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - AOS (advanced orbiting systems) space data link protocol

BS ISO 15396:2007 空间数据和信息传输系统.交互支持参考模型.空间链路扩展业务

This International Standard defines a cross support reference model which provides a common basis for coordinating the development of CCSDS Recommended Standards for space link extension (SLE) service specifications and serves as a reference to maintain the consistency of these Recommended Standards. The scope and field of application are furthermore detailed in subclauses 1.2 and 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems. Cross support reference model. Space link extension services

SAE AIR5682-2007 普通发射适合区域通路的接口控制文献(CLARA ICD)

CLARA identifies four functions: Data Space Generator, Truth Data Generator, Coefficient Generator, and Reconstructor. Together these four functions standardize the solution to the LAR problem. This ICD defines the logical interfaces of the four functions. This document specifies the CLARA interfaces of the Data Space Generator, Truth Data Generator, Coefficient Generator, and Reconstructor functions. The weapon and delivery platform developers define the details of each function. The Data Space Generator selects a representative set of discrete release conditions, (such as altitude, wind, speed, and release flight path angle) from a continuum of release-condition possibilities. For each set of release conditions, the Data Space Generator defines a corresponding grid of target points. The subset from the multi-dimensional space of discrete release conditions, along with their corresponding grid of target points, wind constraints, and impact angle constraints serve as the input to the Truth Data Generator. The Truth Data Generator uses the Data Space Generator output to calculate the achieved impact parameters (velocity, angles, and miss distance). The Truth Database stores the release conditions and the achieved impact parameters for each target point. The Truth Data Generator generates impact data sets for the Coefficient Generator. The Truth Data Generator uses a model of the weapon system that predicts weapon delivery performance to a predefined accuracy. The weapon model may use Six-Degrees-Of-Freedom (6DOF) or another mathematical representation that meets the objective for the weapon system LAR. The Coefficient Generator generates coefficients for a mathematical fitting model. This mathematical fitting model is commonly referred to as the LAR Algorithm. The output of the Reconstructor is an approximation of the original weapon footprint data based on flight and environment conditions. The Mission Planning, Trainer Systems, and weapon delivery aircraft use this approximation.

Common Launch Acceptability Region Approach Interface Control Document (CLARA ICD)

ISO 17355:2007 空间数据和信息传输系统.空间数据系统咨询委员会(CCSDS)文档传送协议

This International Standard defines a CCSDS file delivery protocol (CFDP) and associated service for application in the space environment. It is intended for use over the current and envisaged packet delivery services used in the space environment, including ⎯ CCSDS conventional packet telecommand; ⎯ CCSDS conventional packet telemetry; ⎯ CCSDS advanced orbiting systems (AOS) path service. It may also operate over a wide variety of ground network services, including those specified by the CCSDS for cross-support purposes. The protocol operates in the space-to-ground, ground-to-space, and space-tospace directions of transfer. It may be initiated by the file sending or receiving entity. In the interests of interoperability, protocol elements are included for generalized forms of standard file manipulation operations based on assumptions of a common model for a ‘filestore’, or medium used to store files. It is recognized, however, that the precise nature and capabilities of filestore management systems are operating-system dependent and, for that reason, the protocol assumes a virtual filestore and associated services that an implementation must map to the capabilities of the actual filestore used. The scope and field of application are furthermore detailed in subclauses 1.2 and 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - CCSDS file delivery protocol

ISO 15396:2007 空间数据和信息传输系统.交互支持参考模型.空间链路扩展业务

This International Standard defines a cross support reference model which provides a common basis for coordinating the development of CCSDS Recommended Standards for space link extension (SLE) service specifications and serves as a reference to maintain the consistency of these Recommended Standards. The scope and field of application are furthermore detailed in subclauses 1.2 and 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - Cross support reference model - Space link extension services

GJB 5919-2007 军航管制员工作站界面显示要求

本标准规定了军航管制员工作站界面内容和显示的基本要求。 本标准适用于军航管制员工作站航迹显示及人机界面的设计，军航管制中心系统其它席位的界面设计可参照使用。

Requirement for display of military air traffic controller workstation

ISO 22671:2007 航天数据和信息传送系统.空间链路扩展(SLE).向前通信链路传送装置(CLTU)业务

This International Standard defines the communications link transmission unit (CLTU) service in conformance with the transfer services specified in ISO 15396:1998. The forward CLTU service is a space link extension (SLE) transfer service that enables a mission to send communications link transmission units (CLTUs) to a spacecraft. This International Standard defines, in an abstract manner, the forward CLTU service in terms of - the operations necessary to provide the transfer service; - the parameter data associated with each operation; - the behaviors that result from the invocation of each operation; and - the relationship between, and the valid sequence of, the operations and resulting behaviors. It does not specify - individual implementations or products; - the implementation of entities or interfaces within real systems; - the methods or technologies required to radiate data to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field; - the methods or technologies required for communications; or - the management activities necessary to schedule, configure, and control the forward CLTU service. The scope and field of application are furthermore detailed in subclause 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - Space link extension (SLE) - Forward communications link transmission unit (CLTU) service