Loading…

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...

Full description

Saved in:
Bibliographic Details
Published in:IEEE transactions on aerospace and electronic systems 2023-10, Vol.59 (5), p.1-17
Main Authors: Sun, Jinlin, Pu, Zhiqiang, Chang, Yafei, Ding, Shihong, Yi, Jianqiang
Format: Article
Language:English
Subjects:
Citations: Items that this one cites
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-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03
cites cdi_FETCH-LOGICAL-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03
container_end_page 17
container_issue 5
container_start_page 1
container_title IEEE transactions on aerospace and electronic systems
container_volume 59
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
format article
fullrecord <record><control><sourceid>proquest_ieee_</sourceid><recordid>TN_cdi_proquest_journals_2875582851</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><ieee_id>10121615</ieee_id><sourcerecordid>2875582851</sourcerecordid><originalsourceid>FETCH-LOGICAL-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03</originalsourceid><addsrcrecordid>eNpNkF1LwzAUhoMoOKc_QPCi4HVnPpo0uRxzc8LQC6d3UtL0xGV0TU06dP_elu3Cq8N7eN7D4UHoluAJIVg9rKfztwnFlE0YzTOs5BkaEc7zVAnMztEIYyJTRTm5RFcxbvuYyYyN0Oe0bb1rOqjStdtBMvNNF3ydWB-SRQ2_rqwhWR5aCNE3ziQfsHGmhpj8uG4z0JXrnG90nTy62O1DqRsDyQt86WF9jS6sriPcnOYYvS_m69kyXb0-Pc-mq9RQlXUpF5oqzKuSYkWlsNhSxnKsjJXEGlnqEpgylSBCYE6JLjXLKROWG8is0JiN0f3xbhv89x5iV2z9PvRfxYLKnHNJJSc9RY6UCT7GALZog9vpcCgILgaLxWCxGCwWJ4t95-7YcQDwjyeUCMLZHzuEbow</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2875582851</pqid></control><display><type>article</type><title>Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation</title><source>IEEE Electronic Library (IEL) Journals</source><creator>Sun, Jinlin ; Pu, Zhiqiang ; Chang, Yafei ; Ding, Shihong ; Yi, Jianqiang</creator><creatorcontrib>Sun, Jinlin ; Pu, Zhiqiang ; Chang, Yafei ; Ding, Shihong ; Yi, Jianqiang</creatorcontrib><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><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 &amp; Communications Abstracts</collection><collection>Mechanical &amp; 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>
fulltext fulltext
identifier ISSN: 0018-9251
ispartof IEEE transactions on aerospace and electronic systems, 2023-10, Vol.59 (5), p.1-17
issn 0018-9251
1557-9603
language eng
recordid cdi_proquest_journals_2875582851
source IEEE Electronic Library (IEL) Journals
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
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-25T00%3A00%3A28IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_ieee_&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Appointed-Time%20Control%20for%20Flexible%20Hypersonic%20Vehicles%20with%20Conditional%20Disturbance%20Negation&rft.jtitle=IEEE%20transactions%20on%20aerospace%20and%20electronic%20systems&rft.au=Sun,%20Jinlin&rft.date=2023-10-01&rft.volume=59&rft.issue=5&rft.spage=1&rft.epage=17&rft.pages=1-17&rft.issn=0018-9251&rft.eissn=1557-9603&rft.coden=IEARAX&rft_id=info:doi/10.1109/TAES.2023.3274098&rft_dat=%3Cproquest_ieee_%3E2875582851%3C/proquest_ieee_%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c294t-56a2905db209286f0f233709cf81fc8babe39cd61660521aba37236f5ce4f6a03%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2875582851&rft_id=info:pmid/&rft_ieee_id=10121615&rfr_iscdi=true