Journal of System Simulation
Abstract
Abstract: To cope with cooperative guidance against multiple targets, a distributed cooperative guidance for multigroup flight vehicles to strike multiple targets with separated impact time is proposed. The collaborative variables for multigroup flight vehicles with separated impact time are given, and the guidance law in the line of sight (LOS) is proposed. The guidance laws on the normal and lateral directions of the LOS are proposed to make the LOS deflection angle rate and LOS the inclination angle rate converge rapidly, which ensures that each vehicle is able to strike the target. The finite-time convergence of the proposed guidance laws is proved by theoretical analysis. Simulation results verify the effectiveness of the proposed methods.
Recommended Citation
Li, Guofei; Li, Shituo; Huangfu, Yilun; Hua, Yueyang; Wu, Yunjie; and Zuo, Zongyu
(2025)
"Cooperative Guidance for Multigroup Flight Vehicles Against Multiple Targets with Separated Impact Time,"
Journal of System Simulation: Vol. 37:
Iss.
6, Article 8.
DOI: 10.16182/j.issn1004731x.joss.24-0120
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol37/iss6/8
First Page
1427
Last Page
1434
CLC
TP391.9
Recommended Citation
Li Guofei, Li Shituo, Huangfu Yilun, et al. Cooperative Guidance for Multigroup Flight Vehicles Against Multiple Targets with Separated Impact Time[J]. Journal of System Simulation, 2025, 37(6): 1427-1434.
DOI
10.16182/j.issn1004731x.joss.24-0120
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