Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles
A novel standard trajectory design and tracking guidance used in the multiple active leap maneuver mode for hypersonic glide vehicles (HGVs) is proposed in this paper. First, the dynamic equation and multiconstraint model are first established in the flight path coordinate system. Second, the refere...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2024-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2024/6618732 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1849308221141942272 |
|---|---|
| author | Taotao Zhang Jun Zhang Sen Shen Weiyi Chen |
| author_facet | Taotao Zhang Jun Zhang Sen Shen Weiyi Chen |
| author_sort | Taotao Zhang |
| collection | DOAJ |
| description | A novel standard trajectory design and tracking guidance used in the multiple active leap maneuver mode for hypersonic glide vehicles (HGVs) is proposed in this paper. First, the dynamic equation and multiconstraint model are first established in the flight path coordinate system. Second, the reference drag acceleration-normalized energy (D-e) profile of the multiple active leap maneuver mode is quickly determined by the Newton iterative algorithm with a single design parameter. The range to go error is corrected by the drag acceleration profile update algorithm, and the drag acceleration error of the gliding terminal is corrected by the aerodynamic parameter estimation algorithm. Then, the reference drag acceleration tracking guidance law is designed based on the prescribed performance control method. Finally, the CAV-L vehicle model is used for numerical simulation. The results show that the proposed method can satisfy the design requirements of drag acceleration under multiple active leap maneuver modes, and the reference drag acceleration can be tracked precisely. The adaptability and robustness of the proposed method are verified by the Monte Carlo simulations under various combined deviation conditions. |
| format | Article |
| id | doaj-art-16564aac299f45e28fb56c724f1174d0 |
| institution | Kabale University |
| issn | 1687-5974 |
| language | English |
| publishDate | 2024-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-16564aac299f45e28fb56c724f1174d02025-08-20T03:54:32ZengWileyInternational Journal of Aerospace Engineering1687-59742024-01-01202410.1155/2024/6618732Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of VehiclesTaotao Zhang0Jun Zhang1Sen Shen2Weiyi Chen3College of Weapons EngineeringSchool of AstronauticsCollege of Weapons EngineeringCollege of Weapons EngineeringA novel standard trajectory design and tracking guidance used in the multiple active leap maneuver mode for hypersonic glide vehicles (HGVs) is proposed in this paper. First, the dynamic equation and multiconstraint model are first established in the flight path coordinate system. Second, the reference drag acceleration-normalized energy (D-e) profile of the multiple active leap maneuver mode is quickly determined by the Newton iterative algorithm with a single design parameter. The range to go error is corrected by the drag acceleration profile update algorithm, and the drag acceleration error of the gliding terminal is corrected by the aerodynamic parameter estimation algorithm. Then, the reference drag acceleration tracking guidance law is designed based on the prescribed performance control method. Finally, the CAV-L vehicle model is used for numerical simulation. The results show that the proposed method can satisfy the design requirements of drag acceleration under multiple active leap maneuver modes, and the reference drag acceleration can be tracked precisely. The adaptability and robustness of the proposed method are verified by the Monte Carlo simulations under various combined deviation conditions.http://dx.doi.org/10.1155/2024/6618732 |
| spellingShingle | Taotao Zhang Jun Zhang Sen Shen Weiyi Chen Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles International Journal of Aerospace Engineering |
| title | Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles |
| title_full | Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles |
| title_fullStr | Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles |
| title_full_unstemmed | Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles |
| title_short | Multiple Leap Maneuver Trajectory Design and Tracking Method Based on Prescribed Performance Control during the Gliding Phase of Vehicles |
| title_sort | multiple leap maneuver trajectory design and tracking method based on prescribed performance control during the gliding phase of vehicles |
| url | http://dx.doi.org/10.1155/2024/6618732 |
| work_keys_str_mv | AT taotaozhang multipleleapmaneuvertrajectorydesignandtrackingmethodbasedonprescribedperformancecontrolduringtheglidingphaseofvehicles AT junzhang multipleleapmaneuvertrajectorydesignandtrackingmethodbasedonprescribedperformancecontrolduringtheglidingphaseofvehicles AT senshen multipleleapmaneuvertrajectorydesignandtrackingmethodbasedonprescribedperformancecontrolduringtheglidingphaseofvehicles AT weiyichen multipleleapmaneuvertrajectorydesignandtrackingmethodbasedonprescribedperformancecontrolduringtheglidingphaseofvehicles |