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Fault detection and diagnosis for satellite's attitude control system (ACS) using an interactive multiple model (IMM) approach

The main objective of this paper is development of a fault diagnosis, isolation and detection technique that is constructed based on the interacting multiple model (IMM) algorithm for partial (soft) or total (hard) reaction wheel failures in the spacecraft attitude control system (ACS). Based on dif...

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Main Authors:	Tudoroiu, N., Khorasani, K.
Format:	Conference Proceeding
Language:	English
Subjects:	Fault detection Fault diagnosis Feedback control Power supplies Power system modeling Space vehicles Temperature Torque Voltage Wheels
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creator	Tudoroiu, N. Khorasani, K.
description	The main objective of this paper is development of a fault diagnosis, isolation and detection technique that is constructed based on the interacting multiple model (IMM) algorithm for partial (soft) or total (hard) reaction wheel failures in the spacecraft attitude control system (ACS). Based on different scenarios and assumptions, we develop healthy models of the ACS under various operating conditions and construct faulty modes with respect to temperature changes, power supply line voltage changes, torque variations, and unexpected current variations in each motor axis windings of the reaction wheels. Once a fault mode is detected and isolated, we are capable to develop in certain conditions the recovery procedure through feedback control strategies for the ACS
doi_str_mv	10.1109/CCA.2005.1507309
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Once a fault mode is detected and isolated, we are capable to develop in certain conditions the recovery procedure through feedback control strategies for the ACS</description><subject>Fault detection</subject><subject>Fault diagnosis</subject><subject>Feedback control</subject><subject>Power supplies</subject><subject>Power system modeling</subject><subject>Space vehicles</subject><subject>Temperature</subject><subject>Torque</subject><subject>Voltage</subject><subject>Wheels</subject><issn>1085-1992</issn><issn>2576-3210</issn><isbn>0780393546</isbn><isbn>9780780393547</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2005</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><recordid>eNot0D1PwzAUhWGLD4m2sCOxeKMdUu6N4zgeq4hCpVYMwFy5tlOM3DiKXaQu_HYi0em80zMcQu4R5oggn-p6Mc8B-Bw5CAbygoxyLsqM5QiXZAyiAiYZL8orMkKoeIZS5jdkHOM3AAiB5Yj8LtXRJ2pssjq50FLVGmqc2rchukib0NOokvXeJfsYqUrJpaOxVIc29cHTeIrJHuh0Ub_P6DG6dj8I1LXJ9moAfyw9DL7r_BDBWE-nq81mRlXX9UHpr1ty3Sgf7d15J-Rz-fxRv2brt5dVvVhnGnmeMsYlmLJhVhkBptrpgiuGOy52FWKBpRacc2yw0pqxomAGmSgLoYwUTOXCsAl5-HedtXbb9e6g-tP2_Bv7A09KX8A</recordid><startdate>2005</startdate><enddate>2005</enddate><creator>Tudoroiu, N.</creator><creator>Khorasani, K.</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope></search><sort><creationdate>2005</creationdate><title>Fault detection and diagnosis for satellite's attitude control system (ACS) using an interactive multiple model (IMM) approach</title><author>Tudoroiu, N. ; Khorasani, K.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c152t-3590d6f3ead70d8bc45a31b57b811416c75551f18cc33443d137647ad973a27d3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2005</creationdate><topic>Fault detection</topic><topic>Fault diagnosis</topic><topic>Feedback control</topic><topic>Power supplies</topic><topic>Power system modeling</topic><topic>Space vehicles</topic><topic>Temperature</topic><topic>Torque</topic><topic>Voltage</topic><topic>Wheels</topic><toplevel>online_resources</toplevel><creatorcontrib>Tudoroiu, N.</creatorcontrib><creatorcontrib>Khorasani, K.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan (POP) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Xplore</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Tudoroiu, N.</au><au>Khorasani, K.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Fault detection and diagnosis for satellite's attitude control system (ACS) using an interactive multiple model (IMM) approach</atitle><btitle>Proceedings of 2005 IEEE Conference on Control Applications, 2005. 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ispartof	Proceedings of 2005 IEEE Conference on Control Applications, 2005. CCA 2005, 2005, p.1287-1292
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source	IEEE Xplore All Conference Series
subjects	Fault detection Fault diagnosis Feedback control Power supplies Power system modeling Space vehicles Temperature Torque Voltage Wheels
title	Fault detection and diagnosis for satellite's attitude control system (ACS) using an interactive multiple model (IMM) approach
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