Abstract
In this article, a guidance problem for cooperative salvo attack of multiple missiles against a single stationary target is investigated. The proposed guidance law combines the well-known PNG law and cooperative acceleration command, which is based on the feedback of state error between the current missile and the mean value of participant missiles. The state variable in this paper is used as the approximate calculation of time-to-go. The cooperative acceleration command is designed to adjust the flight path and impact time, which leads the multi-missiles to hit the common target simultaneously. During the engagement, the velocities of missiles are not changed and presetting impact time is not needed. Simulation results show the effectiveness of the proposed guidance law.
| Original language | English |
|---|---|
| Pages | 90-94 |
| Number of pages | 5 |
| Publication status | Published - 2014 |
| Event | Joint International Conference of the 10th China-Japan International Workshop on Information Technology and Control Applications and the 6th International Symposium on Computational Intelligence and Industrial Applications, ITCA and ISCIIA 2014 - Changsha, China Duration: 15 Sept 2014 → 20 Sept 2014 |
Conference
| Conference | Joint International Conference of the 10th China-Japan International Workshop on Information Technology and Control Applications and the 6th International Symposium on Computational Intelligence and Industrial Applications, ITCA and ISCIIA 2014 |
|---|---|
| Country/Territory | China |
| City | Changsha |
| Period | 15/09/14 → 20/09/14 |
Keywords
- Cooperative guidance
- Feedback
- Impact time
- Multi-missiles
- Proportional navigation