Open AccessCompound control method for Anti-Unmanned Aerial Vehicle (UAV) vertical launch missile
Author(s) -
Chang Jiapan,
Yongshan Liu
Publication year - 2021
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 - 10.1088/1742-6596/1786/1/012042
Subject(s) - missile , aerodynamics , aerospace engineering , actuator , air to air missile , computer science , control (management) , simulation , engineering , artificial intelligence
A compound control method with aerodynamic canard and reaction jet is proposed for anti-Unmanned Aerial Vehicle (UAV) vertical launch missile. The purpose of this method is to solve the problem of vertical launch with high angle of attack and low dynamic pressure. This paper first introduces the actuator layout and ignition strategy of reaction jet. Then the model of compound control system is established and compared with aerodynamic control in detail. Simulation studies demonstrate the effectiveness of the proposed method.