V37 操纵系统及其附件 标准查询与下载

IEEE 1554/COR-2013 惯性传感器试验设备,仪器,数据采集,以及分析用推荐性操作规程.勘误表

Errata to Recommended Practice for Inertial Sensor Test Equipment, Instrumentation, Data Acquisition, and Analysis

SAE AIR5682A-2012 普通发射可接受区域接口控制文件(CLARA ICD)

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. 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)

SAE AIR5712A-2012 发射可接收区域法(CLARA)基本原理文档

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This document was developed by the SAE AS-1B5 CLARA Task Group to explain and document background information and decisions with associated rationale made in development of the CLARA Interface Control Document (ICD), AIR5682. This rationale document is published separately to preserve information that is not required or provided in the ICD but may be important to users.

Common Launch Acceptability Region Approach (CLARA)Rationale Document

SAE ARP5284B-2012 TLTV.飞机NLG转向和牵引力保护系统或报警设备.检查,维修和校准要求

To list the documentation required to ensure inspection, maintenance and calibration of the TLTV's aircraft NLG steering and tractive protection systems or alerting devices can be carried out in accordance with the requirements of this document and the referenced standards. To specify inspection, maintenance and calibration requirements and procedures. To specify special tools requirements. To specify training requirements. To specify recording, traceability and acountability requirements.

TLTV - Aircraft NLG Steering and Tractive Force Protection Systems or Alerting Devices - Inspection, Maintenance and Calibration Requirements

SAE AIR5664A-2012 无人系统联合体系结构(JAUS)历史和领域模型

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. The purpose of the SAE Aerospace Information Report (AIR) is tow-fold: to inform the reader of the extent of effort that went into the development of the Joint Architecture for Unmanned Systems (JAUS); and to capture for posterity the domain analysis that provides the underpinnings for the work by the AS-4 Committee (Unmanned Systems).

JAUS History and Domain Model

SAE AIR4253B-2012 带遥控自动驾驶仪飞行控制系统飞机的动系统描述

This SAE Aerospace Information Report (AIR) provides design information of various contemporary aircraft fly-by-wire (FBW) flight control actuation systems that may be useful in the design of future actuation systems for similar applications. It is primarily applicable to manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for future aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.

Description of Actuation Systems for Aircraft with Fly-By-Wire Flight Control Systems

SAE ARP6001-2012 航空宇宙.线传飞控交通和商业用无源侧杆单元通用要求

This SAE Aerospace Recommended Practice (ARP) provides general requirements for a generic "passive" side stick that could be used for fly by wire transport and business aircraft. It addresses the following: The functions to be implemented; the geometric and mechanical characteristics; the mechanical and electrical interfaces; the safety and certification requirements.

Aerospace - Passive Side Stick Unit General Requirements for Fly by Wire Transport and Business

ISO 17107:2011 空间数据和信息传递系统.导航数据信息的XML规范

Space data and information transfer systems - XML specification for navigation data messages

BS DD ISO/TS 12208:2011 航天系统.空间环境(天然和人造的).所观察质子通过GEO长时段的影响和太阳质子的统计模型内置信度选择用指南

Space systems. Space environment (natural and artificial). Observed proton fluences over long duration at GEO and guideline for selection of confidence level in statistical model of solar proton fluences

ISO/TS 12208:2011 航天系统.空间环境(天然和人工).在地球同步轨道长期观测质子通量以及太阳质子通量统计模型置信水平的选择指南

Space systems - Space environment (natural and artificial) - Observed proton fluences over long duration at GEO and guideline for selection of confidence level in statistical model of solar proton fluences

SAE AIR6181-2011 电子驱动力控制系统/飞机接口控制文件

This SAE Aerospace Information Report (AIR) provides guidelines to document the functional and physical interface requirements for the electrical systems (including an EPCS and its components) between a given propulsion system and the aircraft on which the system is installed and the functionality pertinent to each interface. The scope includes civilian aircraft powered by turbofan, turboprop, and turboshaft engines equipped with electronic engine controls. Superseding SAE APR 4874

Electronic Propulsion Control System/Aircraft Interface Control Documents

SAE AS5488A-2011 依附在合适接口上的支线客机牵引杆

This SAE Aerospace Standard (AS) specifies the interface requirements for towbar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as "regional aircraft". Its purpose is to achieve towbar attachment fittings interface standardization by aircraft weight category (which determines towbar forces) in order to ensure that one single type of towbar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different towbar types used. This Aerospace Standard is intended to be applicable to all new models of regional aircraft within the specified maximum ramp weight range, entering service or designed after its date of publication. See Section 3, Effectivity, hereafter. It is not its intent to apply to previously in service regional aircraft models, which present a considerable variety of towbar attachment fittings, However, where deemed appropriate in order to facilitate operation of such aircraft types at airports, simple retrofit modifications are described that may be considered to bring certain in service fittings to be compatible with a towbar head meeting this Aerospace Standard.

Regional Aircraft Towbar Attach Fitting Interface

SAE ARP1915D-2010 飞机牵引杆

This SAE Aerospace Recommended Practice (ARP) outlines the basic general design considerations for transport aircraft tow bars. It does not cover the requirements for tow bars intended for aircraft with a maximum ramp mass (MRW) below 8600 kg (19 000 lb).

Aircraft Tow Bar

KS W ISO 1466:2009 航空器的拉杆操纵手动开关.性能要求

이 표준은 항공기의 직류 28 V와 삼상 115/200 V, 교류 400 Hz 시스템에서

Lever-operated manual switches for aircraft-Performance requirements

NAVY MIL-PRF-24635 E-2009 外部使用的耐风化涂料系统

COATING SYSTEMS, WEATHER-RESISTANT, EXTERIOR USE

BS ISO 15862:2009 航空系统.航天器的运载火箭飞行环境遥感勘测数据处理

Space systems - Launch-vehicle-to-spacecraft flight environments telemetry data processing

SAE AIR5665-2008 无人驾驶系统的结构

This SAE Aerospace Information Report (AIR) describes the Architecture Framework for Unmanned Systems (AFUS).AFUS comprises a Conceptual View, a Capabilities View, and an Interoperability View. The Conceptual View providesdefinitions and background for key terms and concepts used in the unmanned systems domain. The Capabilities Viewuses terms and concepts from the Conceptual View to describe capabilities of unmanned systems and of other entities inthe unmanned systems domain. The Interoperability View provides guidance on how to put it all together in a way thatsupports interoperability.

Architecture Framework for Unmanned Systems

GJB 35B-2008 歼(强)击机座舱几何尺寸

本标准规定了歼(强)击机座舱几何尺寸 本标准适用于单座或串列双座杆式操纵歼击机、强击机、歼击轰炸机及上述飞机的教练机

Aircrew station geometry for fighter and attacker

GJB 6373-2008 机载测控设备标校方法

本标准规定了机载光学设备、惯导设备和卫通天线轴角零值的地面静态标校方法。 本标准适用于机载测控站建设、机载测控通信设备安装位置的测量、设备测量零值和（或）天线指向零值的标定。

Ground calibration methods on airborne TE&C equipments

HB 6486-2008 飞机飞行控制系统名词术语

本标准规定了飞机飞行控制系统的常用技术术语。 本标准适用于飞机飞行控制系统、分系统及其部件的设计、生产和试验，也适用于本领域内的教学、科研和管理。对于未列出的复合名词，可按相应术语组合。

Terms and definitions of aireraft flight control system