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Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation
This paper investigates the anti-disturbance control design for flexible air-breathing hypersonic vehicles (FAHVs) with appointed-time prescribed tracking performances. The challenging issues include multisource disturbances, cross-coupling effects of the vehicle dynamics, and asymmetric amplitude a...
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Published in: | IEEE transactions on aerospace and electronic systems 2023-10, Vol.59 (5), p.1-17 |
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creator | Sun, Jinlin Pu, Zhiqiang Chang, Yafei Ding, Shihong Yi, Jianqiang |
description | This paper investigates the anti-disturbance control design for flexible air-breathing hypersonic vehicles (FAHVs) with appointed-time prescribed tracking performances. The challenging issues include multisource disturbances, cross-coupling effects of the vehicle dynamics, and asymmetric amplitude and rate saturations. To address these issues, we propose an appointed-time prescribed performance control scheme for FAHVs via conditional disturbance negation technique. In contrast to existing disturbance rejection approaches, the proposed control scheme not only estimates the disturbances first in a fixed time, but also evaluates the estimated disturbances and selectively conducts compensation actions according to the insight of the FAHV dynamic characteristics. To further enhance convergence rate, the composite appointed-time prescribed performance controllers are designed for FAHVs via time-varying barrier Lyapunov function and nonsmooth backstepping technique, which ensure satisfactory transient response and steady-state performances. In addition, the asymmetric amplitude and rate saturation problem of actuators are dealt with by introducing unified approximation dynamics. It is rigorously proved that the practical appointed-time convergence of the tracking errors and the fixed-time convergence of all signals in the resultant FAHV closed-loop system can be achieved under the proposed control scheme. Finally, extensive comparative simulations are provided to demonstrate the feasibility and superiority of the proposed approach. |
doi_str_mv | 10.1109/TAES.2023.3274098 |
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The challenging issues include multisource disturbances, cross-coupling effects of the vehicle dynamics, and asymmetric amplitude and rate saturations. To address these issues, we propose an appointed-time prescribed performance control scheme for FAHVs via conditional disturbance negation technique. In contrast to existing disturbance rejection approaches, the proposed control scheme not only estimates the disturbances first in a fixed time, but also evaluates the estimated disturbances and selectively conducts compensation actions according to the insight of the FAHV dynamic characteristics. To further enhance convergence rate, the composite appointed-time prescribed performance controllers are designed for FAHVs via time-varying barrier Lyapunov function and nonsmooth backstepping technique, which ensure satisfactory transient response and steady-state performances. In addition, the asymmetric amplitude and rate saturation problem of actuators are dealt with by introducing unified approximation dynamics. It is rigorously proved that the practical appointed-time convergence of the tracking errors and the fixed-time convergence of all signals in the resultant FAHV closed-loop system can be achieved under the proposed control scheme. Finally, extensive comparative simulations are provided to demonstrate the feasibility and superiority of the proposed approach.</description><identifier>ISSN: 0018-9251</identifier><identifier>EISSN: 1557-9603</identifier><identifier>DOI: 10.1109/TAES.2023.3274098</identifier><identifier>CODEN: IEARAX</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>Actuators ; Aerodynamics ; Amplitudes ; Appointed-time control ; Asymmetry ; Closed loop systems ; Closed loops ; conditional disturbance negation ; Control systems ; Convergence ; Cross coupling ; Disturbances ; Dynamic characteristics ; Feedback control ; hypersonic vehicle ; Hypersonic vehicles ; input saturation ; Liapunov functions ; Mathematical models ; prescribed performance control ; Tracking errors ; Transient response ; Vehicle dynamics</subject><ispartof>IEEE transactions on aerospace and electronic systems, 2023-10, Vol.59 (5), p.1-17</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2023</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03</citedby><cites>FETCH-LOGICAL-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03</cites><orcidid>0000-0002-4841-4048 ; 0000-0003-3268-9482 ; 0000-0002-4509-1124 ; 0000-0003-2297-7050</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/10121615$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,776,780,27903,27904,54774</link.rule.ids></links><search><creatorcontrib>Sun, Jinlin</creatorcontrib><creatorcontrib>Pu, Zhiqiang</creatorcontrib><creatorcontrib>Chang, Yafei</creatorcontrib><creatorcontrib>Ding, Shihong</creatorcontrib><creatorcontrib>Yi, Jianqiang</creatorcontrib><title>Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation</title><title>IEEE transactions on aerospace and electronic systems</title><addtitle>T-AES</addtitle><description>This paper investigates the anti-disturbance control design for flexible air-breathing hypersonic vehicles (FAHVs) with appointed-time prescribed tracking performances. The challenging issues include multisource disturbances, cross-coupling effects of the vehicle dynamics, and asymmetric amplitude and rate saturations. To address these issues, we propose an appointed-time prescribed performance control scheme for FAHVs via conditional disturbance negation technique. In contrast to existing disturbance rejection approaches, the proposed control scheme not only estimates the disturbances first in a fixed time, but also evaluates the estimated disturbances and selectively conducts compensation actions according to the insight of the FAHV dynamic characteristics. To further enhance convergence rate, the composite appointed-time prescribed performance controllers are designed for FAHVs via time-varying barrier Lyapunov function and nonsmooth backstepping technique, which ensure satisfactory transient response and steady-state performances. In addition, the asymmetric amplitude and rate saturation problem of actuators are dealt with by introducing unified approximation dynamics. It is rigorously proved that the practical appointed-time convergence of the tracking errors and the fixed-time convergence of all signals in the resultant FAHV closed-loop system can be achieved under the proposed control scheme. Finally, extensive comparative simulations are provided to demonstrate the feasibility and superiority of the proposed approach.</description><subject>Actuators</subject><subject>Aerodynamics</subject><subject>Amplitudes</subject><subject>Appointed-time control</subject><subject>Asymmetry</subject><subject>Closed loop systems</subject><subject>Closed loops</subject><subject>conditional disturbance negation</subject><subject>Control systems</subject><subject>Convergence</subject><subject>Cross coupling</subject><subject>Disturbances</subject><subject>Dynamic characteristics</subject><subject>Feedback control</subject><subject>hypersonic vehicle</subject><subject>Hypersonic vehicles</subject><subject>input saturation</subject><subject>Liapunov functions</subject><subject>Mathematical models</subject><subject>prescribed performance control</subject><subject>Tracking errors</subject><subject>Transient response</subject><subject>Vehicle dynamics</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNpNkF1LwzAUhoMoOKc_QPCi4HVnPpo0uRxzc8LQC6d3UtL0xGV0TU06dP_elu3Cq8N7eN7D4UHoluAJIVg9rKfztwnFlE0YzTOs5BkaEc7zVAnMztEIYyJTRTm5RFcxbvuYyYyN0Oe0bb1rOqjStdtBMvNNF3ydWB-SRQ2_rqwhWR5aCNE3ziQfsHGmhpj8uG4z0JXrnG90nTy62O1DqRsDyQt86WF9jS6sriPcnOYYvS_m69kyXb0-Pc-mq9RQlXUpF5oqzKuSYkWlsNhSxnKsjJXEGlnqEpgylSBCYE6JLjXLKROWG8is0JiN0f3xbhv89x5iV2z9PvRfxYLKnHNJJSc9RY6UCT7GALZog9vpcCgILgaLxWCxGCwWJ4t95-7YcQDwjyeUCMLZHzuEbow</recordid><startdate>20231001</startdate><enddate>20231001</enddate><creator>Sun, Jinlin</creator><creator>Pu, Zhiqiang</creator><creator>Chang, Yafei</creator><creator>Ding, Shihong</creator><creator>Yi, Jianqiang</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0002-4841-4048</orcidid><orcidid>https://orcid.org/0000-0003-3268-9482</orcidid><orcidid>https://orcid.org/0000-0002-4509-1124</orcidid><orcidid>https://orcid.org/0000-0003-2297-7050</orcidid></search><sort><creationdate>20231001</creationdate><title>Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation</title><author>Sun, Jinlin ; Pu, Zhiqiang ; Chang, Yafei ; Ding, Shihong ; Yi, Jianqiang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Actuators</topic><topic>Aerodynamics</topic><topic>Amplitudes</topic><topic>Appointed-time control</topic><topic>Asymmetry</topic><topic>Closed loop systems</topic><topic>Closed loops</topic><topic>conditional disturbance negation</topic><topic>Control systems</topic><topic>Convergence</topic><topic>Cross coupling</topic><topic>Disturbances</topic><topic>Dynamic characteristics</topic><topic>Feedback control</topic><topic>hypersonic vehicle</topic><topic>Hypersonic vehicles</topic><topic>input saturation</topic><topic>Liapunov functions</topic><topic>Mathematical models</topic><topic>prescribed performance control</topic><topic>Tracking errors</topic><topic>Transient response</topic><topic>Vehicle dynamics</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sun, Jinlin</creatorcontrib><creatorcontrib>Pu, Zhiqiang</creatorcontrib><creatorcontrib>Chang, Yafei</creatorcontrib><creatorcontrib>Ding, Shihong</creatorcontrib><creatorcontrib>Yi, Jianqiang</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Xplore</collection><collection>CrossRef</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>Advanced Technologies Database with Aerospace</collection><jtitle>IEEE transactions on aerospace and electronic systems</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sun, Jinlin</au><au>Pu, Zhiqiang</au><au>Chang, Yafei</au><au>Ding, Shihong</au><au>Yi, Jianqiang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation</atitle><jtitle>IEEE transactions on aerospace and electronic systems</jtitle><stitle>T-AES</stitle><date>2023-10-01</date><risdate>2023</risdate><volume>59</volume><issue>5</issue><spage>1</spage><epage>17</epage><pages>1-17</pages><issn>0018-9251</issn><eissn>1557-9603</eissn><coden>IEARAX</coden><abstract>This paper investigates the anti-disturbance control design for flexible air-breathing hypersonic vehicles (FAHVs) with appointed-time prescribed tracking performances. The challenging issues include multisource disturbances, cross-coupling effects of the vehicle dynamics, and asymmetric amplitude and rate saturations. To address these issues, we propose an appointed-time prescribed performance control scheme for FAHVs via conditional disturbance negation technique. In contrast to existing disturbance rejection approaches, the proposed control scheme not only estimates the disturbances first in a fixed time, but also evaluates the estimated disturbances and selectively conducts compensation actions according to the insight of the FAHV dynamic characteristics. To further enhance convergence rate, the composite appointed-time prescribed performance controllers are designed for FAHVs via time-varying barrier Lyapunov function and nonsmooth backstepping technique, which ensure satisfactory transient response and steady-state performances. In addition, the asymmetric amplitude and rate saturation problem of actuators are dealt with by introducing unified approximation dynamics. It is rigorously proved that the practical appointed-time convergence of the tracking errors and the fixed-time convergence of all signals in the resultant FAHV closed-loop system can be achieved under the proposed control scheme. Finally, extensive comparative simulations are provided to demonstrate the feasibility and superiority of the proposed approach.</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TAES.2023.3274098</doi><tpages>17</tpages><orcidid>https://orcid.org/0000-0002-4841-4048</orcidid><orcidid>https://orcid.org/0000-0003-3268-9482</orcidid><orcidid>https://orcid.org/0000-0002-4509-1124</orcidid><orcidid>https://orcid.org/0000-0003-2297-7050</orcidid></addata></record> |
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subjects | Actuators Aerodynamics Amplitudes Appointed-time control Asymmetry Closed loop systems Closed loops conditional disturbance negation Control systems Convergence Cross coupling Disturbances Dynamic characteristics Feedback control hypersonic vehicle Hypersonic vehicles input saturation Liapunov functions Mathematical models prescribed performance control Tracking errors Transient response Vehicle dynamics |
title | Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation |
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