Open AccessResearch on fast switching interception of the real target
Author(s) -
T. Y. Wang
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1507/8/082024
Subject(s) - interception , terminal guidance , ballistic missile , missile , terminal (telecommunication) , missile guidance , computer science , control theory (sociology) , kinetic energy , energy (signal processing) , mode (computer interface) , terminal sliding mode , trajectory , simulation , aerospace engineering , engineering , sliding mode control , artificial intelligence , physics , nonlinear system , control (management) , ecology , telecommunications , quantum mechanics , astronomy , biology , operating system
In order to distinguish the decoy missile from the real in the middle of the ballistic missile flight, we proposed using image recognition and sliding-mode guidance in the kinetic energy interceptor terminal guidance phase. The paper set background on the kinetic energy interceptor in the middle course of ballistic missile flight. Due to the influence of the dummy target, the preset interception point is out of alignment and interceptors require terminal guidance adjustment. In this paper, two different global fast Terminal sliding modes are used to establish the intercept model equation. By simulink simulation comparison, it is found that the sliding mode guidance proposed in this paper can quickly and effectively switch interception orbit to hit the target.