Loading…
Hardware/software integration & verification for the mobile servicing system of the international space station
The system architecture of the Mobile Service System (MSS) forms an integral part of the architecture of the International Space Station (ISS) in which elements interact through data components controlled by their respective element software. Tne element developers produce software components which,...
Saved in:
Published in: | Acta astronautica 1999, Vol.44 (7), p.391-398 |
---|---|
Main Author: | |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-c339t-c6e4fa201dc54c5b60c2d975c4837c5b3fd8f25a79ad14709e50cc1257f09f333 |
---|---|
cites | |
container_end_page | 398 |
container_issue | 7 |
container_start_page | 391 |
container_title | Acta astronautica |
container_volume | 44 |
creator | Foran, F.L. |
description | The system architecture of the Mobile Service System (MSS) forms an integral part of the architecture of the International Space Station (ISS) in which elements interact through data components controlled by their respective element software. Tne element developers produce software components which, subsequent to being validated on their respective elements, are integrated and verified in test environments which are representative of the integrated MSS/ISS system. This is the classical method for integration and verification. If program software requirements are, for various reasons, slow to finalize, the software development process starts later than anticipated, and following the classical development/verification processes, could put the scheduled software deliveries at risk. A new approach to development and verification is needed which must encompass the entire software program from component unit software to fully integrated system software. This paper describes the approach which was taken to perform system hardware/software integration and verification with software components which were essentially incomplete, but were developed in a phased fashion, having mutually compatible functionality. The paper describes the MSS and ISS system architecture, the various software components and an overview of the original integration and verification plan. The paper will then describe the new integration approach which was developed, and discuss the evolution of the various software components in terms of functionality and their phased integration into a system. The paper will conclude by providing a summary of the results of the integration and verification activities, and demonstrate how delivery schedules for the integrated system software were met. |
doi_str_mv | 10.1016/S0094-5765(99)00085-5 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_744708100</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0094576599000855</els_id><sourcerecordid>744708100</sourcerecordid><originalsourceid>FETCH-LOGICAL-c339t-c6e4fa201dc54c5b60c2d975c4837c5b3fd8f25a79ad14709e50cc1257f09f333</originalsourceid><addsrcrecordid>eNqFkEtPwzAQhC0EEqXwE5B84nEIXSdxHZ8QqnhJlTgAZ8t11sUojYvtFvXfkyaIK6fd0X4z0g4h5wxuGLDp5BVAlhkXU34l5TUAVDzjB2TEKiGzHAo4JKM_5JicxPjZQSKv5Ij4Jx3qbx1wEr1N-4W6NuEy6OR8Sy_oFoOzzgzS-kDTB9KVX7gGacSwdca1Sxp3MeGKetuf9wmh7S26oXGtTcemXp-SI6ubiGe_c0zeH-7fZk_Z_OXxeXY3z0xRyJSZKZZW58Bqw0vDF1MweS0FN2VViE4Xtq5szrWQumalAIkcjGE5FxakLYpiTC6H3HXwXxuMSa1cNNg0ukW_iUqUnatiAB3JB9IEH2NAq9bBrXTYKQZq36_q-1X78pSUqu9X8c53O_iwe2PrMKhoHLYGaxfQJFV790_CDyDfhKQ</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>744708100</pqid></control><display><type>article</type><title>Hardware/software integration & verification for the mobile servicing system of the international space station</title><source>ScienceDirect Journals</source><creator>Foran, F.L.</creator><creatorcontrib>Foran, F.L.</creatorcontrib><description>The system architecture of the Mobile Service System (MSS) forms an integral part of the architecture of the International Space Station (ISS) in which elements interact through data components controlled by their respective element software. Tne element developers produce software components which, subsequent to being validated on their respective elements, are integrated and verified in test environments which are representative of the integrated MSS/ISS system. This is the classical method for integration and verification. If program software requirements are, for various reasons, slow to finalize, the software development process starts later than anticipated, and following the classical development/verification processes, could put the scheduled software deliveries at risk. A new approach to development and verification is needed which must encompass the entire software program from component unit software to fully integrated system software. This paper describes the approach which was taken to perform system hardware/software integration and verification with software components which were essentially incomplete, but were developed in a phased fashion, having mutually compatible functionality. The paper describes the MSS and ISS system architecture, the various software components and an overview of the original integration and verification plan. The paper will then describe the new integration approach which was developed, and discuss the evolution of the various software components in terms of functionality and their phased integration into a system. The paper will conclude by providing a summary of the results of the integration and verification activities, and demonstrate how delivery schedules for the integrated system software were met.</description><identifier>ISSN: 0094-5765</identifier><identifier>EISSN: 1879-2030</identifier><identifier>DOI: 10.1016/S0094-5765(99)00085-5</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Computer hardware ; Computer software ; Mobile robots ; Orbits ; Robotics</subject><ispartof>Acta astronautica, 1999, Vol.44 (7), p.391-398</ispartof><rights>1999</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c339t-c6e4fa201dc54c5b60c2d975c4837c5b3fd8f25a79ad14709e50cc1257f09f333</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,4021,27921,27922,27923</link.rule.ids></links><search><creatorcontrib>Foran, F.L.</creatorcontrib><title>Hardware/software integration & verification for the mobile servicing system of the international space station</title><title>Acta astronautica</title><description>The system architecture of the Mobile Service System (MSS) forms an integral part of the architecture of the International Space Station (ISS) in which elements interact through data components controlled by their respective element software. Tne element developers produce software components which, subsequent to being validated on their respective elements, are integrated and verified in test environments which are representative of the integrated MSS/ISS system. This is the classical method for integration and verification. If program software requirements are, for various reasons, slow to finalize, the software development process starts later than anticipated, and following the classical development/verification processes, could put the scheduled software deliveries at risk. A new approach to development and verification is needed which must encompass the entire software program from component unit software to fully integrated system software. This paper describes the approach which was taken to perform system hardware/software integration and verification with software components which were essentially incomplete, but were developed in a phased fashion, having mutually compatible functionality. The paper describes the MSS and ISS system architecture, the various software components and an overview of the original integration and verification plan. The paper will then describe the new integration approach which was developed, and discuss the evolution of the various software components in terms of functionality and their phased integration into a system. The paper will conclude by providing a summary of the results of the integration and verification activities, and demonstrate how delivery schedules for the integrated system software were met.</description><subject>Computer hardware</subject><subject>Computer software</subject><subject>Mobile robots</subject><subject>Orbits</subject><subject>Robotics</subject><issn>0094-5765</issn><issn>1879-2030</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1999</creationdate><recordtype>article</recordtype><recordid>eNqFkEtPwzAQhC0EEqXwE5B84nEIXSdxHZ8QqnhJlTgAZ8t11sUojYvtFvXfkyaIK6fd0X4z0g4h5wxuGLDp5BVAlhkXU34l5TUAVDzjB2TEKiGzHAo4JKM_5JicxPjZQSKv5Ij4Jx3qbx1wEr1N-4W6NuEy6OR8Sy_oFoOzzgzS-kDTB9KVX7gGacSwdca1Sxp3MeGKetuf9wmh7S26oXGtTcemXp-SI6ubiGe_c0zeH-7fZk_Z_OXxeXY3z0xRyJSZKZZW58Bqw0vDF1MweS0FN2VViE4Xtq5szrWQumalAIkcjGE5FxakLYpiTC6H3HXwXxuMSa1cNNg0ukW_iUqUnatiAB3JB9IEH2NAq9bBrXTYKQZq36_q-1X78pSUqu9X8c53O_iwe2PrMKhoHLYGaxfQJFV790_CDyDfhKQ</recordid><startdate>1999</startdate><enddate>1999</enddate><creator>Foran, F.L.</creator><general>Elsevier Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TC</scope></search><sort><creationdate>1999</creationdate><title>Hardware/software integration & verification for the mobile servicing system of the international space station</title><author>Foran, F.L.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c339t-c6e4fa201dc54c5b60c2d975c4837c5b3fd8f25a79ad14709e50cc1257f09f333</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1999</creationdate><topic>Computer hardware</topic><topic>Computer software</topic><topic>Mobile robots</topic><topic>Orbits</topic><topic>Robotics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Foran, F.L.</creatorcontrib><collection>CrossRef</collection><collection>Mechanical Engineering Abstracts</collection><jtitle>Acta astronautica</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Foran, F.L.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Hardware/software integration & verification for the mobile servicing system of the international space station</atitle><jtitle>Acta astronautica</jtitle><date>1999</date><risdate>1999</risdate><volume>44</volume><issue>7</issue><spage>391</spage><epage>398</epage><pages>391-398</pages><issn>0094-5765</issn><eissn>1879-2030</eissn><abstract>The system architecture of the Mobile Service System (MSS) forms an integral part of the architecture of the International Space Station (ISS) in which elements interact through data components controlled by their respective element software. Tne element developers produce software components which, subsequent to being validated on their respective elements, are integrated and verified in test environments which are representative of the integrated MSS/ISS system. This is the classical method for integration and verification. If program software requirements are, for various reasons, slow to finalize, the software development process starts later than anticipated, and following the classical development/verification processes, could put the scheduled software deliveries at risk. A new approach to development and verification is needed which must encompass the entire software program from component unit software to fully integrated system software. This paper describes the approach which was taken to perform system hardware/software integration and verification with software components which were essentially incomplete, but were developed in a phased fashion, having mutually compatible functionality. The paper describes the MSS and ISS system architecture, the various software components and an overview of the original integration and verification plan. The paper will then describe the new integration approach which was developed, and discuss the evolution of the various software components in terms of functionality and their phased integration into a system. The paper will conclude by providing a summary of the results of the integration and verification activities, and demonstrate how delivery schedules for the integrated system software were met.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/S0094-5765(99)00085-5</doi><tpages>8</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0094-5765 |
ispartof | Acta astronautica, 1999, Vol.44 (7), p.391-398 |
issn | 0094-5765 1879-2030 |
language | eng |
recordid | cdi_proquest_miscellaneous_744708100 |
source | ScienceDirect Journals |
subjects | Computer hardware Computer software Mobile robots Orbits Robotics |
title | Hardware/software integration & verification for the mobile servicing system of the international space station |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T10%3A08%3A07IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Hardware/software%20integration%20&%20verification%20for%20the%20mobile%20servicing%20system%20of%20the%20international%20space%20station&rft.jtitle=Acta%20astronautica&rft.au=Foran,%20F.L.&rft.date=1999&rft.volume=44&rft.issue=7&rft.spage=391&rft.epage=398&rft.pages=391-398&rft.issn=0094-5765&rft.eissn=1879-2030&rft_id=info:doi/10.1016/S0094-5765(99)00085-5&rft_dat=%3Cproquest_cross%3E744708100%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c339t-c6e4fa201dc54c5b60c2d975c4837c5b3fd8f25a79ad14709e50cc1257f09f333%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=744708100&rft_id=info:pmid/&rfr_iscdi=true |