摘要
Aiming at salvo-attack problem of a system of multiple flight vehicles, two event-triggered mechanism-based finite-time consensus cooperative guidance methods are proposed. These methods utilize an event-triggered mechanism to decrease the frequency of control command generation and communication. On this basis, the communication load is lightened, and the effectiveness and reliability are promoted. Firstly, a two-phase guidance scheme is presented. More specifically, the intermediate variables are forced to achieve consensus within a small region around zero during the first phase, and the 3D proportional navigation guidance law is introduced to achieve the accurate guidance during the second phase. Next, the engagement dynamics model of each member of the multi-vehicle system is built and transformed to a second-order multiple-agent system. A terminal sliding manifold is presented to reduce the order. Finally, based on the event-triggered mechanism, centralized and distributed consensus guidance method are proposed, respectively. Theoretical analysis and simulation results demonstrate the properties of effectiveness, finite-time convergence and Zeno-phenomenon avoidance.
投稿的翻译标题 | Even-triggered Mechanism-based Finite-time Consensus Cooperative Guidance Methods for Multiple-vehicle System |
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源语言 | 繁体中文 |
页(从-至) | 946-956 |
页数 | 11 |
期刊 | Yuhang Xuebao/Journal of Astronautics |
卷 | 44 |
期 | 6 |
DOI | |
出版状态 | 已出版 - 6月 2023 |
关键词
- Event-triggered mechanism
- Finite-time consensus
- Multiple vehicles cooperative guidance
- Terminal sliding mode
- Two-phase guidance