Distributed cooperative encirclement hunting guidance method for intercepting maneuvering target

YU Jianglong; DONG Xiwang; LI Qingdong; LYU Jinhu; REN Zhang

doi:10.7527/S1000-6893.2021.25817

ACTA AERONAUTICAET ASTRONAUTICA SINICA >

2022 , Vol. 43 >Issue 9: 325817 - 325817

DOI: https://doi.org/10.7527/S1000-6893.2021.25817

Electronics and Electrical Engineering and Control

Distributed cooperative encirclement hunting guidance method for intercepting maneuvering target

YU Jianglong ,
DONG Xiwang ,
LI Qingdong ,
LYU Jinhu ,
REN Zhang

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1. Science and Technology on Aircraft Control Laboratory, School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China;
2. Institute of Artificial Intelligence, Beihang University, Beijing 100191, China

Received date: 2021-05-15

Revised date: 2021-06-22

Online published: 2021-08-17

Supported by

National Natural Science Foundation of China (62103016, 61922008, 61973013, 61803014, 62103023); Science and Technology Innovation 2030-Key Project of “New Generation Artificial Intelligence” (2020AAA0108200); China National Postdoctoral Program for Innovative Talents (BX20200034); China Postdoctoral Science Foundation (2020M680297)

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Abstract

In this paper, the problem of distributed cooperative encirclement hunting guidance for multiple aircrafts intercepting a maneuvering target in the multi-leader multi-follower mode is studied. Based on the biological mechanism of wolves' cooperative encirclement hunting of large maneuvering prey, three strategies for the cooperative guidance architecture in the leader-follower mode, distributed communication and state estimation, and multi-channel and multi-directional cooperative encirclement hunting guidance Law are abstracted mathematically. Firstly, for the leader-follower cooperative guidance architecture, a cooperative encirclement hunting scheme in the multi-leader multi-follower mode is proposed. Secondly, for multi-leader aircrafts, a cooperative anti-orbit interception guidance law with target’s uncertain maneuver compensation is developed to provide a favorable reference trajectory for the follower aircrafts. For multiple followers, a distributed state observer is used to estimate the convex combination of the state trajectories of multiple leaders. A time-varying encirclement hunting line of line-of-sight formation tracking guidance law is designed by using local information, and a dynamic compensation system is introduced to solve the input saturation problem. Then, the stability analysis of the closed-loop system and the feasibility analysis of the cooperative guidance system are conducted. Finally, the theoretical results are verified by numerical simulation. The simulation results show that it is appropriate for multiple aircrafts to form a certain encirclement hunting configuration on both sides of the target escape direction. That is, there exist several proper terminal guidance interception positions for aircrafts, which can improve maneuvering target interception efficiency.

Key words： cooperative guidance; time-varying formation tracking; encirclement hunting guidance; maneuvering target; anti-orbit interception; leader-follower mode; line of sight formation

Cite this article

YU Jianglong , DONG Xiwang , LI Qingdong , LYU Jinhu , REN Zhang . Distributed cooperative encirclement hunting guidance method for intercepting maneuvering target[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022 , 43(9) : 325817 -325817 . DOI: 10.7527/S1000-6893.2021.25817

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