V07 电子计算机应用 标准查询与下载

SAE AIR1706B-1997 用于稳态分析和初步系统规模确定的高级环境控制系统(AECS)计算机程序

The purpose of this AIR is to provide aircraft ECS engineers and their managers with information about a generalized computer program method for calculating steady state thermodynamic performance of an aircraft environmental control system. Many current computer programs are company proprietary or tend to be specifically oriented to a particular ECS configuration or system. This AIR describes a computer program general enough to allow analysis of essentially all types of environmental control systems. It is available to companies in the environmental control system industry. The general nature of the computer solution is useful for sizing activities and trade study during a preliminary design phase, as well as for detailed system performance analysis. The intent of this AIR is improved communication between aircraft user, aircraft manufacturer, and ECS equipment suppliers by use of an industry-wide computer program. This AIR describes the Advanced Environmental Control System Computer Program, and suggests further improvements to expand its capabilities.

The Advanced Environmental Control System (AECS) Computer Program for Steady State Analysis and Preliminary System Sizing

ISO 13764:1996 空间数据和信息传输系统 标准格式化数据单元 控制权限程序

Lays down the requirements for Control Authority procedures for standard formatted data units used in space systems. Technically identical with CCSDS 630.0.B-1-1993.

Space data and information transfer systems - Standard formatted data units - Control authority procedures

SAE AIR1823A-1996 飞机ECS动态分析的(R)工程分析系统 (EASY)计算程序

The Engineering Analysis System (EASY) computer program is summarized in this report. It provides techniques for analysis of steady-state and dynamic (transient) environmental control system (ECS) performance, control system stability, and for synthesis of optimal ECS. General uses of a transient analysis computer program for ECS design and development, and general features of EASY relative to these uses, are presented. This report summarizes the nine analysis options of EASY, EASY program organization for analyzing ECS, data input to the program and resulting data output, and a discussion of EASY limitations. A generalized computer program for determining transient thermodynamic performance of aircraft ECS, and methods for dynamic analysis of aircraft ECS are discussed in this report.

(R) Engineering Analysis System (EASY) Computer Program for Dynamic Analysis of Aircraft ECS

SAE AS4893-1996 通用开放体系结构(GOA)的框架

This SAE Aerospace Standard (AS) establishes a Generic Open Architecture (GOA) Framework for application independent hardware/software systems. This document defines the interface classes for the GOA Framework. Supplemental documents define the guidelines for applying the GOA Framework to specific applications.

Generic Open Architecture (GOA) Framework

SAE AIR877B-1996 航空.颗粒计数的数据转换和外推

This Aerospace Information Report (AIR) describes a mathematical model that can be used to analyze particle count data. Particle counts that fit the model can be graphically displayed, converted from one counting size-frequency range to another, and extrapolated to estimate counts beyond the measured range. Derivation, applications and calculations are described. Cumulative particle counts larger than stated size-range are fitted against a modified log-normal distribution function by plotting on special log-log graph paper. Many real particle distributions approximate a straight line, showing good fit for this log-normal model. The resultant plot provides a basis for further analysis, including size-range conversion and extrapolation.

Aerospace-Particle Count Data Conversion and Extrapolation

SAE AS8002A-1996 飞行数据计算机的最低性能标准

This SAE Aerospace Standard (AS) covers air data computer equipment (hereinafter designated the computer) which when connected to sources of aircraft electrical power, static pressure, total pressure, outside air temperature, and others specified by the manufacturer (singly or in combination) provides some or all of the following computed air data output signals (in analog and/or digital form) which may supply primary flight instruments: pressure altitude; pressure altitude, baro-corrected; vertical speed; calibrated airspeed; mach number; maximum allowable airspeed; overspeed warning; and total air temperature. In addition, the computer may supply one or more of the following signals: pressure altitude, digitized; equivalent airspeed; true airspeed; static air temperature; altitude hold; airspeed hold; mach hold; angle of attack; flight control gain scheduling; and others.

Air Data Computer - Minimum Performance Standard

HB 7233-1995 民用机载计算机软件质量保证大纲编写指南

本标准规定了民用机载计算机软件质量保证大纲编写的基本要求。 　　本标准适用于民用机载系统或设备软件开发过程中的质量保证。

Guidelines for Compiling Software Quality Assurance Program for Civil Airborne Computers

AC-111-02-1995 民用航空器适航信息管理程序

Civil Aircraft Airworthiness Information Management Program

AP-111-02-1995 民用航空器适航信息管理程序

Civil Aircraft Airworthiness Information Management Program

SAE AIR1855A-1995 导弹和运载车辆的传动系统数据摘要

This SAE Aerospace Information Report (AIR) includes all missile and launch vehicle actuation systems, including electrohydraulic, electropneumatic, and electromechanical types. The data for many systems are not complete. As more information becomes available, periodic updates will be issued to complete existing data sheets and to add new ones. An index by type of vehicle and by type of actuation system is included. The actual data sheets in the body of the report are organized in alphabetical order. A survey of existing designs (past and present) is a valuable aid during the concept formulation stage of a new design. This summary report on missile and launch vehicle actuation systems has been formulated to provide a data base that should be useful in the initial design stages of a new system.

Actuation System Data Summary for Missiles and Launch Vehicles

HB 7127-1994 管理信息系统分析、设计与实施的基本要求

本标准规定了管理信息开发实施的统一要求。 　　本标准适用于管理信息系统开发实施的全过程。

Basic requirements for management information system analysis, design and implementation

AIAA R-023A-1995 为航天系统的运作而设的机器人-计算机界面的推荐作法

The following bounds were applied to the scope of this document

Recommended Practice Human-Computer Interfaces for Space System Operations

ASTM F1591-95 地面发生紧急情况时地勤人员与飞行器中人员之间可视信号的标准规程

1.1 This practice covers the signals to be used between persons on the ground and in aircraft when two-way voice communications cannot be established during ground emergencies. Ground signals are limited to land-based ones that do not require special equipment. Flare, light, panel, and maritime signals are specifically excluded. 1.2 The signals are divided into two categories: those used by persons on the ground and those used by aircraft. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Visual Signals Between Persons on the Ground and in Aircraft During Ground Emergencies

HB 7091-1994 机载设备标准电子模块的设计要求

本标准规定了机载设备标准电子模块的结构（包括机械和电气）、环境、标记和可靠性等设计要求。 　　本标准适用于军用机载设备标准电子模块的设计。

Design Requirements for Standard Electronic Modules of Airborne Equipment

HB 7092-1994 机载设备标准电子模块的采用要求

本标准规定了机载标准电子模块的采用要求。 　　本标准适用于军用机载设备标准电子模块的采用。

Requirements for Adoption of Standard Electronic Modules for Airborne Equipment

HB 7093-1994 飞机座舱电（场）致发光信息板

本标准规定了飞机和直升机座舱内控制板（盒）、操纵台、仪表板用电（场）致发光信息板产品分类、技术要求、试验方法、检验规则及标志、包装、运输、贮存的通用要求。 　　本标准适用于飞机和直升机座舱内的电（场）致发光信息板（以下简称发光板）。

Aircraft cockpit electro (field) luminescence information board

HB/Z 244-1993 软件支持环境

本标准为任务承办单位定义开发软件的支持环境（简称开发环境）规定了一个统一的、最低的要求，以保证该环境和任务委托单位指定的生存周期软件支持环境（即按合同开发的软件所驻留的支持环境，简称生存周期环境）相兼容。 　　本标准适用于所有软件开发环境和生存周期环境为非同一环境的软件项目合同。本标准的各项要求适用于按合同交付的软件及有关的支持软件。

Software Support Environment

HB 6881-1993 计算机制图规定

本标准规定了计算机会制工程图样的画法、简化画法及标注方法。 　　本标准适用于航空产品的机械图样绘制，其他工程图样亦可参照使用。

Computer Graphics Regulations

AECMA PREN 3911-1993 航空航天系列六突出几何凹进定义

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-3.

Aerospace Series Six Lobe Recess Geometrical Definition Edition P 1

SAE AIR4845-1993 同步工程(CE)环境下的故障模式分析程序

This AIR by the G-11AT (automation and Tools) subcommittee, examines the failure mode, effects and criticality analysis (FMECA) requirements and procedures as performed on current and earlier vintage engineering programs. The subcommittee has focused on these procedures in relation to the concurrent engineering (CE) environment to determine where it may be beneficial, to both FMECA analysts and users, to automate some or all of the FMECA processes. Its purpose is to inform the reader about FMECAs and how the FMECA process could be automated in a concurrent engineering environment. There is no intent on the part of the authors that the material presented should become requirements or specifications imposed as part of any future contract. The report is structured to include the following subjects: a. a FMECA overview; b. the current FMECA process; c. FMECA in the concurrent engineering environment; d. FMECA automation; and e. the benefits of automation.

FMECA Process in the Concurrent Engineering (CE) Environment