V73 航天器控制导引系统 标准查询与下载

QJ 3289-2007 地空导弹射频寻的制导控制系统半实物仿真试验要求与方法

本标准规定了射频寻的地空导弹进行制导控制系统半实物仿真试验时的要求和方法。 本标准适用于地空导弹射频寻的制导控制系统半实物仿真试验。

Requirements and methods of hardware-in-the-loop simulation test for radio frequency homing guidance control system of surface-to-air missile

ISO 26143:2007 空间数据和信息传输系统.空间链路扩展(SLE).回程操作控制场业务

This International Standard defines the space link extension (SLE) return operational control fields (ROCF) service in conformance with ISO 15396:1998. The ROCF service is an SLE transfer service that delivers to a mission user all operational control fields from one master channel or one virtual channel. This International Standard defines, in an abstract manner, the ROCF service in terms of - the operations necessary to provide the 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 acquire telemetry frames from signals received from a spacecraft; - the methods or technologies required to provide a suitable environment for communications; or - the management activities required to schedule, configure, and control the ROCF 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) - Return operational control fields service

ISO 22672:2006 航天数据和信息传输系统.空间链路扩展(SLE).正向空间数据包业务

The Forward Space Packet (FSP) service is a Space Link Extension (SLE) transfer service that enables a mission to send Space Packets to a spacecraft in sequence-controlled or expedited mode. This International Standard defines, in an abstract manner, the FSP service in terms of - the operations necessary to provide the transfer service; - the parameter data associated with each operation; - the behaviours that result from the invocation of each operation; - the relationship between, and the valid sequence of, the operations and resulting behaviours. It does not specify - individual implementations or products; - the implementation of entities or interfaces within real systems; - the methods or technologies required to radiate Space Packets 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; - the management activities necessary to schedule, configure, and control the FSP service. The scope and field of application are furthermore detailed in subclauses 1.1 to 1.3 of the enclosed CCSDS publication.

Space data and information transfer systems - Space link extension (SLE) - Forward space packet service

ISO 22644:2006 航天数据和信息传送系统.轨道数据文电

This International Standard specifies two standard message formats for use in transferring spacecraft orbit information between space Agencies: the Orbit Parameter Message (OPM) and the Orbit Ephemeris Message (OEM). Such exchanges are used for - pre-flight planning for tracking or navigation support; - scheduling tracking support; - carrying out tracking operations (sometimes called metric predicts); - performing orbit comparisons; - carrying out navigation operations such as orbit propagation. This International Standard includes sets of requirements and criteria that the message formats have been designed to meet. For exchanges where these requirements do not capture the needs of the participating Agencies another mechanism may be selected. The scope and field of application are furthermore detailed in subclauses 1.1 and 1.2 of the enclosed CCSDS publication.

Space data and information transfer systems - Orbit data messages

NAVY MIL-DTL-18307 H-2006 飞艇驾驶员系统的命名和识别包括联合电子指定系统和相关支撑系统

This specification establishes requirements for obtaining the official assignment or confirmation of nomenclature and for identification and re-identification marking for electronic and aeronautical equipment, including support equipment and systems; e.g., Test, Utility, Trainers, etc. Nomenclature procedures are explained in MIL-STD-196 for electronic equipment and MIL-HDBK-1812 for aeronautical, aeronautical support equipment, and photographic equipment.

NOMENCLATURE AND IDENTIFICATION FOR AERONAUTICAL SYSTEMS INCLUDING JOINT ELECTRONICS TYPE DESIGNATED SYSTEMS AND ASSOCIATED SUPPORT SYSTEMS

ISO 22663:2006 空间数据和信息传输系统.接近1的空间链接协议.数据链路层

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

ISO 15389:2001/cor 1:2006 航天系统.空中到地面的临时管缆.技术勘误1

This standard is Space systems - Flight-to-ground umbilicals; Technical Corrigendum 1.

Space systems - Flight-to-ground umbilicals; Technical Corrigendum 1

GJB 1306A-2005 战略导弹测试发射控制系统设备通用规范

本规范规定了战略导弹测试发射控制系统设备的要求、质量保证规定和交货准备。 本规范适用于战略导弹测试发射控制系统设备(以下简称设备)的研制、生产和验收。

General specification for equipments of test and firing control system of strategic missiles

GJB 5476-2005 反坦克导弹电视测角装置规范

本规范规定了反坦克导弹电视测角装置的要求、质量保证规定和交货准备等内容。 本规范适用于发坦克导弹电视测角装置（以下简称为电视测角装置）的设计、制造与验收。

Specificationg for anti-Tank missile CCD video goniometer

QJ 3211-2005 混合集成电路HB2824S12、HB2815D45 DC/DC变换器详细规范

本规范规定了厚膜混合集成电路HB2824S12和HB2815D45两种DC/DC变换器（以下简称变换器）的技术要求、质量保证规定和交货准备等。 本规范适用于变换器的研制、生产、采购和使用。

Detail specification for hybrid integrated type HB2824S12、HB2815D45 DC/DC converters

QJ 3207-2005 电视导引头通用规范

本规范规定了电视导引头的通用技术要求、质量保证规定和交货准备。 本规范适用于电视导引头的研制、设计、制造、试验和验收。

General specification for TV seeker

QJ 2802A-2005 飞航导弹调频连续波无线电高度表设计准则和方法

本标准规定了飞航导弹用调频连续波无线电高度表在设计中应遵循的设计依据、设计准则、设计程序及内容、设计方法以及设计验证试验项目与要求等。 本标准适用于飞航导弹用调频连续波无线电高度表（以下简称高度表）的设计。

Design criteria and method for FM/CW radio altimeter of cruise missiles

QJ 2113A-2005 海防导弹雷达导引头通用规范

本规范规定了海防导弹主动雷达导引头（以下简称雷达）的要求、质量保证规定、交货准备和说明事项等。 本规范适用于岸-舰、舰-舰、潜-舰、空-舰导弹雷达的设计、制造、试验和验收。

General specification for defence for sea dafence missile homing head radar

ARMY ADS-20-HDBK-2005 军用飞机武器装备和火力控制系统调查

This handbook is for guidance only. Do not cite this document as a requirement.

ARMAMENT AND FIRE CONTROL SYSTEM SURVEY FOR ARMY AIRCRAFT

QJ 2616A-2004 石英谐振器筛选要求

Screen requiremints of quartz crystal unit

QJ 2277A-2004 地地导弹控制系统发射阵地测试方法

Launch site testing method for control system of ground missiles

QJ 2150A-2004 飞航导弹射击指挥仪测试方法

Test methods for control panel of crusise missile

QJ 1458A-2004 气浮陀螺平台测试方法

Test method of platform based air-suspension gyrocsope

QJ 1079A-2004 陀螺仪主要精度指标和测试方法

Major precision parameters and testing methods for gyroscopes

ISO 17401:2004 航天系统.运载工具用航天飞行器接口要求文献

This International Standard provides spacecraft (SC) organizations with the general format for presenting the interface requirement document (IRD) for launch vehicle services. The IRD provides a list of the major technical requirements spacecraft agencies provide to launch vehicle (LV) agencies when submitting an application for launch services. The IRD addresses the definition of the SC mission, the mechanical and electrical interfaces, the overall environment requirements (mechanical, thermal, cleanliness, radio-electrical), the SC development and test programme and, finally, launch range facilities and support requirements. This International Standard is applicable to all existing commercial LV and related launch facilities so as to permit SC contractors to prepare a single interface requirement document for a given SC mission, independently of the LV contractor to be selected. The IRD, as defined in this International Standard, includes the basic SC input data needed by LV agencies to prepare the interface control document defined in the ISO 15863.

Space systems - Spacecraft interface requirements document for launch vehicle services