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...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
IEEE
2019-01-01
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| Series: | IEEE Access |
| Subjects: | |
| Online Access: | https://ieeexplore.ieee.org/document/8809704/ |
| _version_ | 1818911303620624384 |
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| author | Yang Gao Guangbin Cai Xiaogang Yang Mingzhe Hou |
| author_facet | Yang Gao Guangbin Cai Xiaogang Yang Mingzhe Hou |
| author_sort | Yang Gao |
| collection | DOAJ |
| 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. |
| first_indexed | 2024-12-19T22:56:34Z |
| format | Article |
| id | doaj.art-15ad062599cd428685d7ac813df71f4a |
| institution | Directory Open Access Journal |
| issn | 2169-3536 |
| language | English |
| last_indexed | 2024-12-19T22:56:34Z |
| publishDate | 2019-01-01 |
| publisher | IEEE |
| record_format | Article |
| series | IEEE Access |
| spelling | doaj.art-15ad062599cd428685d7ac813df71f4a2022-12-21T20:02:37ZengIEEEIEEE Access2169-35362019-01-01711924611925810.1109/ACCESS.2019.29369748809704Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone ConstraintYang Gao0https://orcid.org/0000-0001-9828-0618Guangbin Cai1Xiaogang Yang2Mingzhe Hou3College of Missile Engineering, Rocket Force University of Engineering, Xi’an, ChinaCollege of Missile Engineering, Rocket Force University of Engineering, Xi’an, ChinaCollege of Missile Engineering, Rocket Force University of Engineering, Xi’an, ChinaSchool of Astronautics, Harbin Institute of Technology, Harbin, ChinaAn 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.https://ieeexplore.ieee.org/document/8809704/Tentacle-based guidanceno-fly zone(NFZ)flight constraintwarning areahypersonic vehicle |
| spellingShingle | Yang Gao Guangbin Cai Xiaogang Yang Mingzhe Hou Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint IEEE Access Tentacle-based guidance no-fly zone(NFZ) flight constraint warning area hypersonic vehicle |
| title | Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint |
| title_full | Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint |
| title_fullStr | Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint |
| title_full_unstemmed | Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint |
| title_short | Improved Tentacle-Based Guidance for Reentry Gliding Hypersonic Vehicle With No-Fly Zone Constraint |
| title_sort | improved tentacle based guidance for reentry gliding hypersonic vehicle with no fly zone constraint |
| topic | Tentacle-based guidance no-fly zone(NFZ) flight constraint warning area hypersonic vehicle |
| url | https://ieeexplore.ieee.org/document/8809704/ |
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