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Studies on Multi-Constraints Cooperative Guidance Method Based on Distributed MPC for Multi-Missiles
| Content Provider | MDPI |
|---|---|
| Author | Cong, Mingyu Cheng, Xianghong Zhao, Zhiquan Li, Zhijun |
| Copyright Year | 2021 |
| Description | Cooperative terminal guidance with impact angle constraint is a key technology to achieve a saturation attack and improve combat effectiveness. The present study envisaged cooperative terminal guidance with impact angle constraint for multiple missiles. In this pursuit, initially, the three-dimensional cooperative terminal guidance law with multiple constraints was studied. The impact time cooperative strategy of virtual leader missile and follower missiles was designed by introducing virtual leader missiles. Subsequently, based on the distributed model prediction control combined with the particle swarm optimization algorithm, a cooperative terminal guidance algorithm was designed for multiple missiles with impact angle constraint that met the guidance accuracy. Finally, the effectiveness of the algorithm was verified using simulation experiments. |
| Starting Page | 10857 |
| e-ISSN | 20763417 |
| DOI | 10.3390/app112210857 |
| Journal | Applied Sciences |
| Issue Number | 22 |
| Volume Number | 11 |
| Language | English |
| Publisher | MDPI |
| Publisher Date | 2021-11-17 |
| Access Restriction | Open |
| Subject Keyword | Applied Sciences Industrial Engineering Cooperative Guidance Model Prediction Control Multi-missile Cooperative Control Multi-constraint Cooperative Guidance |
| Content Type | Text |
| Resource Type | Article |
