TY - JOUR
T1 - Event-Triggered Cooperative Guidance for Salvo Attack With Impact Vector and Field-of-View Constraints
AU - He, Zhichuan
AU - Wang, Jiang
AU - Li, Hongyan
AU - Liu, Zichao
AU - Lin, Defu
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2026
Y1 - 2026
N2 - In this article, we investigate the 3-D cooperative salvo problem under field-of-view (FOV) constraints and without active speed control. An impact vector control guidance (IVCG) law is proposed by introducing a unified auxiliary variable that integrates the lead angle and the 3-D impact angle error, ensuring their simultaneous convergence. To improve time-to-go estimation performance, a physics-guided neural network (PGNN) is developed to provide high-precision prediction with reduced online computational demand. Furthermore, two sequential bias terms are incorporated into the IVCG law to achieve simultaneous arrival with reduced communication frequency while strictly satisfying the FOV constraint. The main advantage of the proposed approach is that it handles multiconstraint guidance for varying-speed missiles, with better time-to-go prediction than deep neural network and physical models, and lower computational and communication costs than numerical integration and sampled communication. Numerical simulations demonstrate the effectiveness and comparative performance of the proposed cooperative guidance law.
AB - In this article, we investigate the 3-D cooperative salvo problem under field-of-view (FOV) constraints and without active speed control. An impact vector control guidance (IVCG) law is proposed by introducing a unified auxiliary variable that integrates the lead angle and the 3-D impact angle error, ensuring their simultaneous convergence. To improve time-to-go estimation performance, a physics-guided neural network (PGNN) is developed to provide high-precision prediction with reduced online computational demand. Furthermore, two sequential bias terms are incorporated into the IVCG law to achieve simultaneous arrival with reduced communication frequency while strictly satisfying the FOV constraint. The main advantage of the proposed approach is that it handles multiconstraint guidance for varying-speed missiles, with better time-to-go prediction than deep neural network and physical models, and lower computational and communication costs than numerical integration and sampled communication. Numerical simulations demonstrate the effectiveness and comparative performance of the proposed cooperative guidance law.
KW - Cooperative guidance
KW - event-triggered control
KW - impact vector control
KW - physics-guided neural network (PGNN)
UR - https://www.scopus.com/pages/publications/105047496913
U2 - 10.1109/TAES.2026.3721801
DO - 10.1109/TAES.2026.3721801
M3 - Article
AN - SCOPUS:105047496913
SN - 0018-9251
VL - 62
SP - 15459
EP - 15477
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
ER -