Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint
An improved tentacle-based bank-angle transient method that requires less computation and provides effective feedback is proposed to offer a new choice for reentry gliding hypersonic vehicle maneuvering guidance. The longitudinal guidance strategy of hypersonic vehicles is applied to track standard...
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| Veröffentlicht in: | IEEE access 2019, Vol.7, p.119246-119258 |
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| creator | Gao, Yang Cai, Guangbin Yang, Xiaogang Hou, Mingzhe |
| description | An improved tentacle-based bank-angle transient method that requires less computation and provides effective feedback is proposed to offer a new choice for reentry gliding hypersonic vehicle maneuvering guidance. The longitudinal guidance strategy of hypersonic vehicles is applied to track standard trajectories, and the improved tentacle-based bank angle transient lateral strategy avoids static or dynamic no-fly zones. The proposed lateral strategy generates three tentacles for detection, addresses numerical heading angle limitations or no-fly zone constraints, and provides control commands through a time-counting filter. Dispersed cases are verified for static no-fly zones, and a warning area is proposed to avoid dynamic no-fly zones. For dynamic no-fly zones, the velocity and initial position of the no-fly zone are discussed in terms of the impact on the guidance. Finally, the guidance strategy is tested on a high-performance Common Aero Vehicle model in many flights, and all results for the constraints and computation time indicate that the improved tentacle-based guidance method is effective for avoiding no-fly zones where some information is unknown. |
| doi_str_mv | 10.1109/ACCESS.2019.2936974 |
| format | Article |
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The longitudinal guidance strategy of hypersonic vehicles is applied to track standard trajectories, and the improved tentacle-based bank angle transient lateral strategy avoids static or dynamic no-fly zones. The proposed lateral strategy generates three tentacles for detection, addresses numerical heading angle limitations or no-fly zone constraints, and provides control commands through a time-counting filter. Dispersed cases are verified for static no-fly zones, and a warning area is proposed to avoid dynamic no-fly zones. For dynamic no-fly zones, the velocity and initial position of the no-fly zone are discussed in terms of the impact on the guidance. 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(IEEE) 2019</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c408t-5208033a57e8126f237f4adad3cbcef0eed83b61963251f0e542b869d141ce2c3</citedby><cites>FETCH-LOGICAL-c408t-5208033a57e8126f237f4adad3cbcef0eed83b61963251f0e542b869d141ce2c3</cites><orcidid>0000-0001-9828-0618</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/8809704$$EHTML$$P50$$Gieee$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,860,2096,4010,27610,27900,27901,27902,54908</link.rule.ids></links><search><creatorcontrib>Gao, Yang</creatorcontrib><creatorcontrib>Cai, Guangbin</creatorcontrib><creatorcontrib>Yang, Xiaogang</creatorcontrib><creatorcontrib>Hou, Mingzhe</creatorcontrib><title>Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint</title><title>IEEE access</title><addtitle>Access</addtitle><description>An improved tentacle-based bank-angle transient method that requires less computation and provides effective feedback is proposed to offer a new choice for reentry gliding hypersonic vehicle maneuvering guidance. 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Finally, the guidance strategy is tested on a high-performance Common Aero Vehicle model in many flights, and all results for the constraints and computation time indicate that the improved tentacle-based guidance method is effective for avoiding no-fly zones where some information is unknown.</description><subject>Aerodynamics</subject><subject>Alliances</subject><subject>Computation</subject><subject>flight constraint</subject><subject>Gliding</subject><subject>Guidance (motion)</subject><subject>Heating systems</subject><subject>hypersonic vehicle</subject><subject>Hypersonic vehicles</subject><subject>no-fly zone(NFZ)</subject><subject>Strategy</subject><subject>Tentacle-based guidance</subject><subject>Time factors</subject><subject>Trajectory</subject><subject>Transient analysis</subject><subject>Vehicle dynamics</subject><subject>warning area</subject><issn>2169-3536</issn><issn>2169-3536</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><sourceid>ESBDL</sourceid><sourceid>RIE</sourceid><sourceid>DOA</sourceid><recordid>eNpNUdtKAzEQXURB0X6BLwGft-ayySaPddFaEAXrBXwJaTJrU-qmJluhf2_qijgvcz1nhjlFcU7wmBCsLidNcz2fjykmakwVE6quDooTSoQqGWfi8F98XIxSWuFsMpd4fVLY2ccmhi9w6Am63tg1lFcm5XS69c50FlAbInqE3Iw7NF1757t3dLvbQEyh8xa9wNJnFHr1_RLdh_JmvUNvoQPUhC710fiuPyuOWrNOMPr1p8XzzfVTc1vePUxnzeSutBWWfckplpgxw2uQhIqWsrqtjDOO2YWFFgM4yRaCKMEoJznnFV1IoRypiAVq2WkxG3hdMCu9if7DxJ0OxuufQojv2sR-f60m3DgsKFfKuopKIbmrjZWEubYmeWvmuhi48nc-t5B6vQrb2OXzNa04FxTzWuUpNkzZGFKK0P5tJVjvxdGDOHovjv4VJ6POB5QHgD-ElFjVuGLfWUOKQw</recordid><startdate>2019</startdate><enddate>2019</enddate><creator>Gao, Yang</creator><creator>Cai, Guangbin</creator><creator>Yang, Xiaogang</creator><creator>Hou, Mingzhe</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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The longitudinal guidance strategy of hypersonic vehicles is applied to track standard trajectories, and the improved tentacle-based bank angle transient lateral strategy avoids static or dynamic no-fly zones. The proposed lateral strategy generates three tentacles for detection, addresses numerical heading angle limitations or no-fly zone constraints, and provides control commands through a time-counting filter. Dispersed cases are verified for static no-fly zones, and a warning area is proposed to avoid dynamic no-fly zones. For dynamic no-fly zones, the velocity and initial position of the no-fly zone are discussed in terms of the impact on the guidance. 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| subjects | Aerodynamics Alliances Computation flight constraint Gliding Guidance (motion) Heating systems hypersonic vehicle Hypersonic vehicles no-fly zone(NFZ) Strategy Tentacle-based guidance Time factors Trajectory Transient analysis Vehicle dynamics warning area |
| title | Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint |
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