Event-triggered-based distributed differential game guidance laws

To reduce computational loads and save communication resources of multi-missile systems, event-triggered-based distributed differential game guidance laws for the nonlinear cooperative multi-missile system are investigated. First, the cooperative multi-missile interception problem is converted into multi-player zero-sum differential games, where all missiles minimize the cost function while the target maximizes the cost function. Second, event-triggered conditions are designed, for implementing the proposed guidance laws, Adaptive Dynamic Programming technique is adopted to approximate the couple event-triggered Hamilton-Jacobi–Isaacs equation, and adaptive weight-tuning laws are proposed. Furthermore, the proposed guidance laws can guarantee the stability of the nonlinear multi-missile system, which is proved by Lyapunov theory. The estimated weights of neural network and consensus tracking errors are ensured to be Uniformly Ultimately Bounded. Besides, a minimal inter-sample time is established to avoid the Zeno behavior. Finally, experiments show that the number of controller updates can be reduced to 65.36% by the proposed algorithm.

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Publication Details

Journal
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
Published
2024-09-12
DOI
https://doi.org/10.1177/09544100241277236
Citations
1
Primary Topic
Guidance and Control Systems
Type
article
Field-Weighted Citation Impact
1.30
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article

Event-triggered-based distributed differential game guidance laws

Yuanli Cai, Axing Xi
1 citations
Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering
Guidance and Control Systems
1.30
article

Event-triggered-based distributed differential game guidance laws

Yuanli Cai, Axing Xi
article en
1 citations

Abstract

To reduce computational loads and save communication resources of multi-missile systems, event-triggered-based distributed differential game guidance laws for the nonlinear cooperative multi-missile system are investigated. First, the cooperative multi-missile interception problem is converted into multi-player zero-sum differential games, where all missiles minimize the cost function while the target maximizes the cost function. Second, event-triggered conditions are designed, for implementing the proposed guidance laws, Adaptive Dynamic Programming technique is adopted to approximate the couple event-triggered Hamilton-Jacobi–Isaacs equation, and adaptive weight-tuning laws are proposed. Furthermore, the proposed guidance laws can guarantee the stability of the nonlinear multi-missile system, which is proved by Lyapunov theory. The estimated weights of neural network and consensus tracking errors are ensured to be Uniformly Ultimately Bounded. Besides, a minimal inter-sample time is established to avoid the Zeno behavior. Finally, experiments show that the number of controller updates can be reduced to 65.36% by the proposed algorithm.

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace EngineeringVol. 238(16)
Xi'an Jiaotong University (CN)
Openalex Percentile: Top 13%
Guidance and Control Systems
1.30
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Event-triggered-based distributed differential game guidance laws — Yuanli Cai, Axing Xi · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering (2024) | TGRS Research Map | TGRS