JIS X0141-2004 软件测量程序
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来源:标准资料网
【英文标准名称】:Softwaremeasurementprocess
【原文标准名称】:软件测量程序
【标准号】:JISX0141-2004
【标准状态】:作废
【国别】:日本
【发布日期】:2004-06-20
【实施或试行日期】:
【发布单位】:日本工业标准调查会(JP-JISC)
【起草单位】:TechnicalCommitteeonInformationTechnology
【标准类型】:()
【标准水平】:()
【中文主题词】:
【英文主题词】:
【摘要】:この規格は,プロジェクト全体又は組細における測定の仕組みの中でソフトウェアの測定を特定,定義,選択,適用及び改善するために必要なアクティビティ及びタスクを明確にする。この規格は,また,ソフトウニア業界で共通に使用する測定用語の定義も与える。この規格は,ソフトウェアに関する測定量の一覧でもないし,ソフトウニアプロジェクトに適用するための測定量の推奨セットを提供するものでもない。この規格は,特定の情報ニーズに着目した場合,それに適した一連の測定量を定義するためのプロセスを明確にする。
【中国标准分类号】:L77
【国际标准分类号】:35_080
【页数】:42P;A4
【正文语种】:日语
Product Code:SAE AIR1703
Title:In-Flight Thrust Determination
Issuing Committee:E-33 In Flight Propulsion Measurement Committee
Scope: This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1)* Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.
Rationale: This report reviews the major aspects of processes that may be used for the determination of in-flight thrust. It includes discussions of basic definitions, analytical and ground-test methods to predict installed thrust of a given propulsion system, and methods to gather data and calculate thrust of the propulsion system during the flight development program of the aircraft. Much of the treatment is necessarily brief due to space limitations. This document and the British Ministry/Industry Drag Analysis Panel (MIDAP) Guide, which SAE Committee E-33 used as a starting point, can be used to understand the processes and limitations involved in the determination of in-flight thrust. (1.1)* Application to a specific in-flight thrust determination program will require the use of many important assumptions not fully developed herein, and these assumptions must be evaluated during the conduct of the program.
