Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles
This paper addresses the analytical formation control and cooperative guidance problem for multiple hypersonic gliding vehicles under distributed communication. The gliding flight of the hypersonic gliding vehicle is divided into formation control phase and time coordination phase. In formation cont...
Saved in:
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2020-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2020/8826968 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832552556229820416 |
|---|---|
| author | Shengwei Jia Xiao Wang Fugui Li Yulin Wang |
| author_facet | Shengwei Jia Xiao Wang Fugui Li Yulin Wang |
| author_sort | Shengwei Jia |
| collection | DOAJ |
| description | This paper addresses the analytical formation control and cooperative guidance problem for multiple hypersonic gliding vehicles under distributed communication. The gliding flight of the hypersonic gliding vehicle is divided into formation control phase and time coordination phase. In formation control phase, based on the idea of path tracking, the formation controller is designed using the second-order consensus protocol with normal positions as the coordination variables. In time coordination phase, based on the quasi-equilibrium gliding condition and the assumption of uniform deceleration motion, the analytical expression of time to go is derived. Then, the cooperative guidance method is developed using the first-order consensus protocol with time to go as the coordination variable. The proposed method takes full consideration of the characteristics of hypersonic gliding vehicle, such as complex nonlinear dynamics, no thrust, and quasi-equilibrium gliding condition, and no online numerical iteration is needed, which is well applicable for hypersonic gliding vehicles. Simulation results demonstrate the effectiveness of the formation control and cooperative guidance method. |
| format | Article |
| id | doaj-art-33a7728ee91545bb960eaa1e76ffb106 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2020-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-33a7728ee91545bb960eaa1e76ffb1062025-02-03T05:58:25ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742020-01-01202010.1155/2020/88269688826968Distributed Analytical Formation Control and Cooperative Guidance for Gliding VehiclesShengwei Jia0Xiao Wang1Fugui Li2Yulin Wang3Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaChina Academy of Launch Vehicle Technology, Beijing 100076, ChinaChina Academy of Launch Vehicle Technology, Beijing 100076, ChinaInstitute of Remote-sensing Satellite, China Academy of Space Technology, Beijing 100094, ChinaThis paper addresses the analytical formation control and cooperative guidance problem for multiple hypersonic gliding vehicles under distributed communication. The gliding flight of the hypersonic gliding vehicle is divided into formation control phase and time coordination phase. In formation control phase, based on the idea of path tracking, the formation controller is designed using the second-order consensus protocol with normal positions as the coordination variables. In time coordination phase, based on the quasi-equilibrium gliding condition and the assumption of uniform deceleration motion, the analytical expression of time to go is derived. Then, the cooperative guidance method is developed using the first-order consensus protocol with time to go as the coordination variable. The proposed method takes full consideration of the characteristics of hypersonic gliding vehicle, such as complex nonlinear dynamics, no thrust, and quasi-equilibrium gliding condition, and no online numerical iteration is needed, which is well applicable for hypersonic gliding vehicles. Simulation results demonstrate the effectiveness of the formation control and cooperative guidance method.http://dx.doi.org/10.1155/2020/8826968 |
| spellingShingle | Shengwei Jia Xiao Wang Fugui Li Yulin Wang Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles International Journal of Aerospace Engineering |
| title | Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles |
| title_full | Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles |
| title_fullStr | Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles |
| title_full_unstemmed | Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles |
| title_short | Distributed Analytical Formation Control and Cooperative Guidance for Gliding Vehicles |
| title_sort | distributed analytical formation control and cooperative guidance for gliding vehicles |
| url | http://dx.doi.org/10.1155/2020/8826968 |
| work_keys_str_mv | AT shengweijia distributedanalyticalformationcontrolandcooperativeguidanceforglidingvehicles AT xiaowang distributedanalyticalformationcontrolandcooperativeguidanceforglidingvehicles AT fuguili distributedanalyticalformationcontrolandcooperativeguidanceforglidingvehicles AT yulinwang distributedanalyticalformationcontrolandcooperativeguidanceforglidingvehicles |