Distributed Guidance for Multi-wave Arrivals of Multiple Missiles

Coordinating multiple missiles to arrive in structured waves, where missiles within each wave arrive simultaneously and successive waves are separated by specified time intervals, offers substantial operational advantages but remains challenging under distributed information architectures. To address this, this paper proposes a distributed guidance framework for multi-wave arrivals of multiple missiles, bridging the gap between existing simultaneous and sequential impact strategies. An auxiliary coordination variable is introduced, derived from locally estimated arrival times, whose consensus facilitates both intra-wave synchronization and inter-wave spacing. Missile acceleration components along and normal to the line-of-sight are designed to regulate arrival timing and achieve high terminal accuracy. Numerical simulations demonstrate the effectiveness of the proposed approach in representative multi-wave engagement scenarios.

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Publication Details

Journal
Guidance Navigation and Control
Published
2025-10-31
DOI
https://doi.org/10.1142/s2737480725500414
Primary Topic
Guidance and Control Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

Distributed Guidance for Multi-wave Arrivals of Multiple Missiles

Guidance Navigation and Control
Guidance and Control Systems
article

Distributed Guidance for Multi-wave Arrivals of Multiple Missiles

article en

Abstract

Coordinating multiple missiles to arrive in structured waves, where missiles within each wave arrive simultaneously and successive waves are separated by specified time intervals, offers substantial operational advantages but remains challenging under distributed information architectures. To address this, this paper proposes a distributed guidance framework for multi-wave arrivals of multiple missiles, bridging the gap between existing simultaneous and sequential impact strategies. An auxiliary coordination variable is introduced, derived from locally estimated arrival times, whose consensus facilitates both intra-wave synchronization and inter-wave spacing. Missile acceleration components along and normal to the line-of-sight are designed to regulate arrival timing and achieve high terminal accuracy. Numerical simulations demonstrate the effectiveness of the proposed approach in representative multi-wave engagement scenarios.

Guidance Navigation and ControlVol. 06(01)
Beijing Institute of Technology (CN), Beihang University (CN)
Openalex Percentile: Top 33%
Guidance and Control Systems
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Distributed Guidance for Multi-wave Arrivals of Multiple Missiles · Guidance Navigation and Control (2025) | TGRS Research Map | TGRS