V41 导航通讯系统与设备 标准查询与下载

SJ 20936-2005 空降兵指挥自动化系统指挥短语与编码

本标准规定了空降兵指挥自动化系统指挥短语传输信息格式、模板格式、编码及填写要求。 本标准适用于空降兵指挥自动化系统指挥短语的拟制、传输和存储，其他军（兵）种也可参照使用。

Command phrase and code for automated command system of airborn force

SJ 20935-2005 空降兵指挥自动化系统验收规范

本规范规定了空降兵指挥自动化系统检验验收的责任、依据、分类、项目、方法、规则及条件等。 本规范适用于空降兵各级、各类指挥自动化系统和系统配套设备的检验与验收。

Acceptance specification for automated command system of airborn force

SJ 20934-2005 空降兵指挥自动化系统通用要求

本标准规定了空降兵各类各级指挥自动化系统的通用要求。 本标准适用于空降兵各类各级指挥自动化系统的论证、研制和使用。

General requirement for automated command system of the airborn force

GJB 1185A-2005 机载惯性导航系统通用规范

本规范规定了机载惯性导航系统(以下简称惯导系统)的技术要求、质量保证规定和交货准备。 本规范适用于设计、制造、检验和交付。

General specification for airborne inertial navigation system

GJB 5438-2005 瞄准吊舱中央控制计算机通用规范

本规范规定了固定翼飞机瞄准吊舱中央控制计算机分系统的技术要求、质量保证和交货准备等通用要求。 本规范适用于固定翼飞机瞄准吊舱中央控制计算机分系统（以下简称计算机）。

General specification for central control computer of targeting pod

GJB 5428-2005 飞机乘员应急离机信号传输系统通用规范

本规范规定了弹射座椅型乘员应急离机信号传输系统（以下简称信号传输系统）的通用技术要求、质量保证规定和交货准备等。 本规范适用于弹射座椅型成员应急离机信号系统中信号传输系统的设计、制造、鉴定和验收。空中加油、弹射和靶机等系统中的类似系统可参照使用。

General specification for signal transmission systems of the aircrew automated escape

GJB 5435-2005 机载有源矩阵液晶显示器光度和色度测量方法

本标准规定了机载有源矩阵液晶显示器（以下简称显示器）的光度、色度。疵点和亮度动态响应等特性的测量方法。 本标准适用于军用飞机座舱中的直接观察式显示器，也适用于军用直升机座舱中的直接观察式显示器。其它类型的直接观察式平板显示器也可参照使用。

Photometric and colorimetric measurement procedure for airborne active matrix liquid crystal display

GJB 5437-2005 瞄准吊舱光学系统通用设计要求

本标准规定了固定翼飞机瞄准吊舱光学系统的设计依据、设计准则、设计内容和方法，以及设计验证项目等通用要求。 本标准适用于固定翼飞机瞄准吊舱光学系统（以下简称光学系统）的总体设计、理论设计和工程设计。

General design requirements for optical system of targeting pod

SAE ARP5825-2005 双模式室外灯的设计要求和试验过程

This SAE Aerospace Recommended Practice (ARP) contains the general requirements and test procedures for Dual Mode (NVIS Friendly Visible and Covert) exterior lighting for most rotorcraft and fixed wing aircraft and could be applicable to ground vehicles that desire a Dual Mode lighting system.

Design Requirements and Test Procedures for Dual Mode Exterior Lights

ISO 22671:2005 航天数据和信息传输系统.空间链路扩展(SLE).发送指令链路传输装置(CLTU)

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

GJB 5356-2005 航天精密角振动台通用规范

本规范规定了航天精密角振动台的技术要求、质量保证规定和交货准备。 本规范适用于惯性仪表及惯性系统测试用的单轴精密角振动台（以下简称角振动台）的设计、制造和检验。多轴精密角振动台亦可参照使用。

General specification for precision angle vibration table of aerospace

GJB 5385-2005 机载彩色视频摄录像系统规范

本规范规定了机载彩色视频摄录系统（以下简称摄录系统）的要求、质量保证规定和交货准备等内容。 本规范适用于摄录系统的设计、制造、试验和验收。

Specification for airborne color video photographic recording system

GJB 5357-2005 解调分系统通用规范

本规范规定了PCM-FM遥测解调分系统（以下简称解调分系统）的技术要求、质量保证规定和交货准备。 本规范适用于解调分系统的设计、制造、试验和验收。

General specififcation for demodulation subsystem

SAE ARP5628-2005 降落飞机距离间隔控制系统

This document recommends design criteria for the flight deck Final Approach Spacing System (FASS). The FASS is a combination of hardware and software that is required to perform the Final Approach Spacing Function. The FASS is designed to enhance the operational efficiency of flight by providing the crew with a means to obtain a precise aircraft-to-aircraft arrival interval at the runway threshold during instrument approach operations. The FASS provides operationally acceptable speed guidance, appropriate crew alerting, and must be highly reliable and thoroughly responsive to the operational requirements and environment.

Final Approach Spacing System (FASS)

IEEE 1431-2004 科氏振动陀螺仪用IEEE标准规范格式指南和试验过程

Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A standard specification format guide for the preparation of a single-axis CVG is provided. A compilation of recommended procedures for testing a CVG, derived from those presently used in the industry, is also provided. Informative annexes cover CVG design features and theoretical principles of operation.

IEEE Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros

SAE AIR5924-2004 有运输类飞机系统的电子发动机控制系统的集成指南

This SAE Aerospace Information Report (AIR) provides methodologies and approaches that have been used to install and integrate full-authority-digital-engine-control (FADEC) systems on transport category aircraft. Although the information provided is based on turbofan engines installed on large commercial transports, many of the issues raised are equally applicable to corporate, general aviation, regional and commuter aircraft, and to military installations, particularly when commercial aircraft are employed by military users. The word ?engine? is used to designate the aircraft propulsion system. The engine station designations used in this report are shown in Figure 1. Most of the material concerns an Electronic Engine Control (EEC) with its associated software, and its functional integration with the aircraft. However, the report also addresses the physical environment associated with the EEC and its associated wiring and sensors. Since most of today?s transport category engines use dual-channel full-authority digital engine control (FADEC) systems, this is the configuration which is primarily addressed. A typical FADEC system configuration is shown in Figure 2. Special considerations that pertain to single-channel FADEC systems or limited authority ?supervisory? control systems are also addressed.

Guidelines for the Integration of Electronic Engine Control Systems with Transport Category Aircraft Systems

SAE ARP5621-2004 导航信息(图表)的电子显示

The objective of this ARP is to provide a set of user-centered design guidelines for the implementation of data driven electronic aeronautical charts, which dynamically create charts from a database of individual elements. The data driven chart is intended to provide information required to navigate, but it is not intended to supplant the aircraft?s primary navigation display. These guidelines seek to provide a balance between standardization of equipment with similar intended functions and individual manufacturer innovation. This ARP provides guidelines for the display of an electronic chart that can replace existing paper. This document addresses what information is required, when it is required, and how it should be displayed and controlled. This document does not include all the detailed specifications required to generate an electronic aeronautical chart. This document primarily addresses the human factors aspects of electronic chart display, and does not address the software, hardware or system integrity/availability issues associated with certification of an electronic chart system. During the transition to data driven charts, the guidelines of this document should be applied to interim electronic chart products that may be pre-composed, such as vector or raster based electronic charts. This document is designed primarily for IFR Aeronautical Charts. There is a limited discussion of its applicability to VFR charts.

Electronic Display of Aeronautical Information (Charts)

DIN EN 61823:2003 机场照明和航路信用电气设备.AGL系列变压器

Electrical installations for lighting and beaconing of aerodromes - AGL series transformers (IEC 61823:2002, modified); German version EN 61823:2003

BS EN 61823:2003 机场照明和信标导航用电气设备.AGL系列变压器

This standard specifies the characteristics of aeronautical ground lighting series transformers (AGLST) used in aeronautical ground lighting for 6,6 A series circuits, at a service voltage of up to 5 kV, supplied by constant current regulators up to 30 kVA in rating. AGL series transformers provide power to airport lighting luminaires or other loads (resistive) from their secondary circuits. The AGL series transformers provide continuity of the series circuit in the event of a loss of the load on the transformer, and electrical isolation between the primary circuit supplied by a constant current regulator, and the secondary circuit connected to the load under conditions defined in this standard. An AGL series transformer is be able to withstand a permanent short or open-circuit secondary series circuit. Specifications for similar series transformers intended for any primary or secondary currents other than 6,6 A, or to supply alternative voltages, constant power, reactive loads, etc., are not included in this standard.

Electrical installations for lighting and beaconing of aerodromes - AGL series transformers

BS EN 61822:2003 机场照明和信标导航用电气装置.恒流调节器

This International Standard specifies the requirements for a Constant Current Regulator (CCR) having a nominal output of 6,6 A for use in an aeronautical ground lighting constant current series circuit. However CCRs may be manufactured which have a different power rating (kVA) and current steps than those specified in this standard Text deleted. This standard shall be applied where appropriate for these CCRs.

Electrical installations for lighting and beaconing of aerodromes - Constant current regulators