Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints
In this paper, a novel two-stage cooperative homing guidance law with impact-angle and FOV constraints for intercepting a stationary target is investigated. The design for the cooperative stage is based on a multi-agent consensus algorithm to achieve consensus on the time- to-go and the lead angle a...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2023-03, Vol.46 (3), p.590-599 |
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container_title | Journal of guidance, control, and dynamics |
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creator | Yang, Xiaoyan Zhang, Yuchen Song, Shenmin |
description | In this paper, a novel two-stage cooperative homing guidance law with impact-angle and FOV constraints for intercepting a stationary target is investigated. The design for the cooperative stage is based on a multi-agent consensus algorithm to achieve consensus on the time- to-go and the lead angle at the switching time. In the lead-angle- profile tracking stage, two different desired lead-angle profiles are presented. By nullifying the tracking error, objectives such as the terminal impact angle and salvo attack are satisfied. The FOV constraint is maintained during the two phases. The achievable impact sets are obtained analytically under different initial lead angles and limited acceleration command conditions. The remarkable contributions of the proposed approach can be summarized as follows: 1) A multiconstraint cooperative homing guidance law without parameter optimization is investigated. The FOV constraint in both phases is addressed by a constrained multi-agent consensus algorithm and lead-angle-profile tracking control theory. 2) The acceleration command becomes zero at the interception time, and the problem of a guidance command singularity is avoided when the lead angle becomes zero. 3) The achievable impact sets are obtained analytically to ensure proper selection of the desired impacts. |
doi_str_mv | 10.2514/1.G007040 |
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The design for the cooperative stage is based on a multi-agent consensus algorithm to achieve consensus on the time- to-go and the lead angle at the switching time. In the lead-angle- profile tracking stage, two different desired lead-angle profiles are presented. By nullifying the tracking error, objectives such as the terminal impact angle and salvo attack are satisfied. The FOV constraint is maintained during the two phases. The achievable impact sets are obtained analytically under different initial lead angles and limited acceleration command conditions. The remarkable contributions of the proposed approach can be summarized as follows: 1) A multiconstraint cooperative homing guidance law without parameter optimization is investigated. The FOV constraint in both phases is addressed by a constrained multi-agent consensus algorithm and lead-angle-profile tracking control theory. 2) The acceleration command becomes zero at the interception time, and the problem of a guidance command singularity is avoided when the lead angle becomes zero. 3) The achievable impact sets are obtained analytically to ensure proper selection of the desired impacts.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G007040</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Aeronautics ; Algorithms ; Angle of attack ; Communication ; Constraints ; Control theory ; Design ; Error analysis ; Field of view ; Guidance (motion) ; Homing ; Interception ; Kinematics ; Lead angle ; Missiles ; Multiagent systems ; Systems stability ; Tracking control ; Tracking errors</subject><ispartof>Journal of guidance, control, and dynamics, 2023-03, Vol.46 (3), p.590-599</ispartof><rights>Copyright © 2022 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c257t-8244933ce6b7cb43bd4a9c371c49f607b0982952c213617309bea30a7e4203d33</citedby><cites>FETCH-LOGICAL-c257t-8244933ce6b7cb43bd4a9c371c49f607b0982952c213617309bea30a7e4203d33</cites><orcidid>0000-0001-5559-7164</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Yang, Xiaoyan</creatorcontrib><creatorcontrib>Zhang, Yuchen</creatorcontrib><creatorcontrib>Song, Shenmin</creatorcontrib><title>Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints</title><title>Journal of guidance, control, and dynamics</title><description>In this paper, a novel two-stage cooperative homing guidance law with impact-angle and FOV constraints for intercepting a stationary target is investigated. The design for the cooperative stage is based on a multi-agent consensus algorithm to achieve consensus on the time- to-go and the lead angle at the switching time. In the lead-angle- profile tracking stage, two different desired lead-angle profiles are presented. By nullifying the tracking error, objectives such as the terminal impact angle and salvo attack are satisfied. The FOV constraint is maintained during the two phases. The achievable impact sets are obtained analytically under different initial lead angles and limited acceleration command conditions. The remarkable contributions of the proposed approach can be summarized as follows: 1) A multiconstraint cooperative homing guidance law without parameter optimization is investigated. The FOV constraint in both phases is addressed by a constrained multi-agent consensus algorithm and lead-angle-profile tracking control theory. 2) The acceleration command becomes zero at the interception time, and the problem of a guidance command singularity is avoided when the lead angle becomes zero. 3) The achievable impact sets are obtained analytically to ensure proper selection of the desired impacts.</description><subject>Aeronautics</subject><subject>Algorithms</subject><subject>Angle of attack</subject><subject>Communication</subject><subject>Constraints</subject><subject>Control theory</subject><subject>Design</subject><subject>Error analysis</subject><subject>Field of view</subject><subject>Guidance (motion)</subject><subject>Homing</subject><subject>Interception</subject><subject>Kinematics</subject><subject>Lead angle</subject><subject>Missiles</subject><subject>Multiagent systems</subject><subject>Systems stability</subject><subject>Tracking control</subject><subject>Tracking errors</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNotkEFPAjEUhBujiYge_AdNPHkovvZ16fZIiCAJiQdQj02328UlsLtuuxL-vYvwLpO8fJmZDCGPHEYi4fKFj-YACiRckQFPEBmmqbwmA1DIWQIabsldCFsAjmOuBuRrfajZKtqNp9O6bnxrY_nr6bwrc1s5T1ex__jNkR7K-E0X-8a6yCbVZueprXI6K_0uZ3XBPkt_6B2q0PNlFcM9uSnsLviHiw7Jx-x1PX1jy_f5YjpZMicSFVkqpNSIzo8z5TKJWS6tdqi4k7oYg8pAp0Inwon_vgg68xbBKi8FYI44JE9n36atfzofotnWXVv1kUao06WoVU89nynX1iG0vjBNW-5tezQczGk3w81lN_wD71Ndxg</recordid><startdate>202303</startdate><enddate>202303</enddate><creator>Yang, Xiaoyan</creator><creator>Zhang, Yuchen</creator><creator>Song, Shenmin</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0001-5559-7164</orcidid></search><sort><creationdate>202303</creationdate><title>Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints</title><author>Yang, Xiaoyan ; Zhang, Yuchen ; Song, Shenmin</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c257t-8244933ce6b7cb43bd4a9c371c49f607b0982952c213617309bea30a7e4203d33</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Aeronautics</topic><topic>Algorithms</topic><topic>Angle of attack</topic><topic>Communication</topic><topic>Constraints</topic><topic>Control theory</topic><topic>Design</topic><topic>Error analysis</topic><topic>Field of view</topic><topic>Guidance (motion)</topic><topic>Homing</topic><topic>Interception</topic><topic>Kinematics</topic><topic>Lead angle</topic><topic>Missiles</topic><topic>Multiagent systems</topic><topic>Systems stability</topic><topic>Tracking control</topic><topic>Tracking errors</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Yang, Xiaoyan</creatorcontrib><creatorcontrib>Zhang, Yuchen</creatorcontrib><creatorcontrib>Song, Shenmin</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Yang, Xiaoyan</au><au>Zhang, Yuchen</au><au>Song, Shenmin</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2023-03</date><risdate>2023</risdate><volume>46</volume><issue>3</issue><spage>590</spage><epage>599</epage><pages>590-599</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>In this paper, a novel two-stage cooperative homing guidance law with impact-angle and FOV constraints for intercepting a stationary target is investigated. The design for the cooperative stage is based on a multi-agent consensus algorithm to achieve consensus on the time- to-go and the lead angle at the switching time. In the lead-angle- profile tracking stage, two different desired lead-angle profiles are presented. By nullifying the tracking error, objectives such as the terminal impact angle and salvo attack are satisfied. The FOV constraint is maintained during the two phases. The achievable impact sets are obtained analytically under different initial lead angles and limited acceleration command conditions. The remarkable contributions of the proposed approach can be summarized as follows: 1) A multiconstraint cooperative homing guidance law without parameter optimization is investigated. The FOV constraint in both phases is addressed by a constrained multi-agent consensus algorithm and lead-angle-profile tracking control theory. 2) The acceleration command becomes zero at the interception time, and the problem of a guidance command singularity is avoided when the lead angle becomes zero. 3) The achievable impact sets are obtained analytically to ensure proper selection of the desired impacts.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.G007040</doi><tpages>10</tpages><orcidid>https://orcid.org/0000-0001-5559-7164</orcidid></addata></record> |
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subjects | Aeronautics Algorithms Angle of attack Communication Constraints Control theory Design Error analysis Field of view Guidance (motion) Homing Interception Kinematics Lead angle Missiles Multiagent systems Systems stability Tracking control Tracking errors |
title | Two-Stage Cooperative Guidance Strategy with Impact-Angle and Field-of-View Constraints |
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