Nonlinear optimal sliding mode midcourse controller with thrust vector control

A nonlinear midcourse missile controller with thrust vector control (TVC) inputs for the interception of a theater ballistic missile is presented. First, an optimal midcourse guidance law is designed to minimize the control effort and the distance between the missile and the target. Then, a quaterni...

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Hauptverfasser:	Fu-Kuang Yeh, Hsiuan-Hau Chien, Fu, Li-Chen
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Acceleration Applied sciences Computer science Computer science control theory systems Control theory. Systems Equations Exact sciences and technology Force control Missiles Optimal control Quaternions Sliding mode control Space vehicles Target tracking
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creator	Fu-Kuang Yeh Hsiuan-Hau Chien Fu, Li-Chen
description	A nonlinear midcourse missile controller with thrust vector control (TVC) inputs for the interception of a theater ballistic missile is presented. First, an optimal midcourse guidance law is designed to minimize the control effort and the distance between the missile and the target. Then, a quaternion-based sliding-mode attitude controller is proposed to track the attitude command and to cope with the effects from variations of missile's inertia, aerodynamic force, and wind gusts. The exponential stability of the overall system is analyzed thoroughly via Lyapunov stability theory. Extensive simulations are conducted to validate the effectiveness of the proposed guidance law and the associated TVC.
doi_str_mv	10.1109/ACC.2002.1023208
format	Conference Proceeding
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Systems</subject><subject>Equations</subject><subject>Exact sciences and technology</subject><subject>Force control</subject><subject>Missiles</subject><subject>Optimal control</subject><subject>Quaternions</subject><subject>Sliding mode control</subject><subject>Space vehicles</subject><subject>Target tracking</subject><issn>0743-1619</issn><issn>2378-5861</issn><isbn>0780372980</isbn><isbn>9780780372986</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2002</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNpFkEtLAzEYRYMPsK3uBTfZ6G7ql2TyWsrgC0rd6HpIMxkbSSc1ySj-ewutuLqLc7hwL0KXBOaEgL69a5o5BaBzApRRUEdoQplUFVeCHKMpSAVMUq3gBE1A1qwigugzNM35A4BoLWCClss4BD84k3DcFr8xAefgOz-8403sHN74zsYxZYdtHEqKIbiEv31Z47JOYy74y9kS0x89R6e9CdldHHKG3h7uX5unavHy-NzcLSpPpShVXduaCbICw0xNYKWp4lZDb53QK24p6y2XUhkuuLK6VsBV73rRk9pKbk3HZuhm37tN8XN0ubQbn60LwQwujrmlkivFOd2J1wfRZGtCn8xgfW63aTc1_bSES8I1gZ13tfe8c-4f749lv1ZPan4</recordid><startdate>2002</startdate><enddate>2002</enddate><creator>Fu-Kuang Yeh</creator><creator>Hsiuan-Hau Chien</creator><creator>Fu, Li-Chen</creator><general>IEEE</general><scope>6IE</scope><scope>6IH</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIO</scope><scope>IQODW</scope><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>2002</creationdate><title>Nonlinear optimal sliding mode midcourse controller with thrust vector control</title><author>Fu-Kuang Yeh ; Hsiuan-Hau Chien ; Fu, Li-Chen</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i276t-44c4361b0a3a410b9285c90fce69b5c23fc5778a5658c948058fef6f14c75cad3</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2002</creationdate><topic>Acceleration</topic><topic>Applied sciences</topic><topic>Computer science</topic><topic>Computer science; control theory; systems</topic><topic>Control theory. Systems</topic><topic>Equations</topic><topic>Exact sciences and technology</topic><topic>Force control</topic><topic>Missiles</topic><topic>Optimal control</topic><topic>Quaternions</topic><topic>Sliding mode control</topic><topic>Space vehicles</topic><topic>Target tracking</topic><toplevel>online_resources</toplevel><creatorcontrib>Fu-Kuang Yeh</creatorcontrib><creatorcontrib>Hsiuan-Hau Chien</creatorcontrib><creatorcontrib>Fu, Li-Chen</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 Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP) 1998-present</collection><collection>Pascal-Francis</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Fu-Kuang Yeh</au><au>Hsiuan-Hau Chien</au><au>Fu, Li-Chen</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Nonlinear optimal sliding mode midcourse controller with thrust vector control</atitle><btitle>Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301)</btitle><stitle>ACC</stitle><date>2002</date><risdate>2002</risdate><volume>2</volume><spage>1348</spage><epage>1353 vol.2</epage><pages>1348-1353 vol.2</pages><issn>0743-1619</issn><eissn>2378-5861</eissn><isbn>0780372980</isbn><isbn>9780780372986</isbn><abstract>A nonlinear midcourse missile controller with thrust vector control (TVC) inputs for the interception of a theater ballistic missile is presented. First, an optimal midcourse guidance law is designed to minimize the control effort and the distance between the missile and the target. Then, a quaternion-based sliding-mode attitude controller is proposed to track the attitude command and to cope with the effects from variations of missile's inertia, aerodynamic force, and wind gusts. The exponential stability of the overall system is analyzed thoroughly via Lyapunov stability theory. 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source	IEEE Electronic Library (IEL) Conference Proceedings
subjects	Acceleration Applied sciences Computer science Computer science control theory systems Control theory. Systems Equations Exact sciences and technology Force control Missiles Optimal control Quaternions Sliding mode control Space vehicles Target tracking
title	Nonlinear optimal sliding mode midcourse controller with thrust vector control
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