Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle
In order to meet the time and angle requirements of hypersonic glide vehicle’s cooperative reentry, a multi-constraint cooperative reentry trajectory planning algorithm is proposed considering the process constraints and transition point constraints. Time constraints and angle constraints are decomp...
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| Format: | Article |
| Language: | zho |
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Editorial Office of Aero Weaponry
2022-10-01
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| Series: | Hangkong bingqi |
| Subjects: | |
| Online Access: | https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00097.pdf |
| _version_ | 1828085926173081600 |
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| author | Wang Xinyu, Liang Xuezhi, Shi Rui, Zhang Dong |
| author_facet | Wang Xinyu, Liang Xuezhi, Shi Rui, Zhang Dong |
| author_sort | Wang Xinyu, Liang Xuezhi, Shi Rui, Zhang Dong |
| collection | DOAJ |
| description | In order to meet the time and angle requirements of hypersonic glide vehicle’s cooperative reentry, a multi-constraint cooperative reentry trajectory planning algorithm is proposed considering the process constraints and transition point constraints. Time constraints and angle constraints are decomposed to vertical plane and horizontal plane, and Newton iteration method is used to plan drag acceleration-energy profile to achieve the longitudinal trajectory satisfied time and distance constraints. The sequential quadratic programming method is used to search the heeling angle turning point to make the trajectory terminal satisfy angle constraints. Through multiple iteration updates, it can get three-dimensional trajectory satisfied the constraints of time and angle. On this basis, this paper analyzes the flight capability of a single aircraft, and gives the determination method of the coordination parameters. The numerical simulation results show that the proposed method can be applied in various scenarios such as cooperative strike and cooperative delivery, and can plan a three-dimensional trajectory with high time and high angle accuracy for aircrafts. This method has strong adaptability to the mission and can meet various constraints and cooperative requirements. |
| first_indexed | 2024-04-11T04:47:38Z |
| format | Article |
| id | doaj.art-46f8ff6ab48f4fa4b8b71f44ac97caad |
| institution | Directory Open Access Journal |
| issn | 1673-5048 |
| language | zho |
| last_indexed | 2024-04-11T04:47:38Z |
| publishDate | 2022-10-01 |
| publisher | Editorial Office of Aero Weaponry |
| record_format | Article |
| series | Hangkong bingqi |
| spelling | doaj.art-46f8ff6ab48f4fa4b8b71f44ac97caad2022-12-27T08:35:34ZzhoEditorial Office of Aero WeaponryHangkong bingqi1673-50482022-10-0129511010.12132/ISSN.1673-5048.2022.0097Collaborative Trajectory Planning Method for Hypersonic Glide VehicleWang Xinyu, Liang Xuezhi, Shi Rui, Zhang Dong01. School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China;2. Systems Engineering Research Institute, China State Shipbuilding Corporation Limited, Beijing 100081, ChinaIn order to meet the time and angle requirements of hypersonic glide vehicle’s cooperative reentry, a multi-constraint cooperative reentry trajectory planning algorithm is proposed considering the process constraints and transition point constraints. Time constraints and angle constraints are decomposed to vertical plane and horizontal plane, and Newton iteration method is used to plan drag acceleration-energy profile to achieve the longitudinal trajectory satisfied time and distance constraints. The sequential quadratic programming method is used to search the heeling angle turning point to make the trajectory terminal satisfy angle constraints. Through multiple iteration updates, it can get three-dimensional trajectory satisfied the constraints of time and angle. On this basis, this paper analyzes the flight capability of a single aircraft, and gives the determination method of the coordination parameters. The numerical simulation results show that the proposed method can be applied in various scenarios such as cooperative strike and cooperative delivery, and can plan a three-dimensional trajectory with high time and high angle accuracy for aircrafts. This method has strong adaptability to the mission and can meet various constraints and cooperative requirements.https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00097.pdf|hypersonic glide vehicle|collaborative reentry|trajectory planning|time collaboration|direction collaboration|collaborative strategy |
| spellingShingle | Wang Xinyu, Liang Xuezhi, Shi Rui, Zhang Dong Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle Hangkong bingqi |hypersonic glide vehicle|collaborative reentry|trajectory planning|time collaboration|direction collaboration|collaborative strategy |
| title | Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle |
| title_full | Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle |
| title_fullStr | Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle |
| title_full_unstemmed | Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle |
| title_short | Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle |
| title_sort | collaborative trajectory planning method for hypersonic glide vehicle |
| topic | |hypersonic glide vehicle|collaborative reentry|trajectory planning|time collaboration|direction collaboration|collaborative strategy |
| url | https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2022-00097.pdf |
| work_keys_str_mv | AT wangxinyuliangxuezhishiruizhangdong collaborativetrajectoryplanningmethodforhypersonicglidevehicle |