Cooperative time-varying formation guidance for leader-following missiles to intercept a maneuvering target with switching topologies

Author:

Zhao Qilun,Dong XiwangORCID,Song Xun,Ren Zhang

Funder

National Natural Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Cited by 38 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. An Optimization Method of Attitude Control Parameters Based on Genetic Algorithm for the Boost-Glide Rocket;IEEE Transactions on Aerospace and Electronic Systems;2024-08

2. Cooperative Guidance for Simultaneous Interception Using Multiple Sliding Surfaces;2024 European Control Conference (ECC);2024-06-25

3. Robust Cooperative Formation Tracking Guidance for Uncertain Missile Systems;2024 IEEE 18th International Conference on Control & Automation (ICCA);2024-06-18

4. Control Allocation for Spin Interceptor with Aerodynamics and Lateral Thrust Blended;Springer Aerospace Technology;2024

5. Three-Dimensional Cooperative Guidance Law Against Maneuvering Target with Time-Varying Communication Delays;International Journal of Aeronautical and Space Sciences;2023-11-13

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