Research on Multi-missile Cooperative Guidance Law Based on Second-order Sliding Mode Control
LIU Yue1, ZHANG Jialiang2, ZHAO Lijuan2, ZHEN Ziyang1
1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, Jiangsu, China；
2. Shanghai Electro-Mechanical Engineering Institute,Shanghai 201109, China
Abstract：The paper proposes a cooperative guidance law with constraints on guidance time and attack angle in twodimension plane, which can improve the penetration ability and combat effectiveness of multi-missile systems and adapt to the complex and changeable future warfare. By applying the second-order sliding mode control theory and using the backstepping method to ensure the stability of the system, through setting the trajectory of the expected attack angle, the cooperative guidance law with multiple constraints is derived. The guidance law is simulated under the condition that the target is stationary or moving. The guidance law can complete the cooperative guidance task with time and angle constraints within a certain limit range of lateral acceleration.
刘悦, 张佳梁, 赵利娟, 甄子洋. 基于二阶滑模控制的多导弹协同制导律研究[J]. 空天防御, 2020, 3(3): 83-88.
LIU Yue, ZHANG Jialiang, ZHAO Lijuan, ZHEN Ziyang. Research on Multi-missile Cooperative Guidance Law Based on Second-order Sliding Mode Control. Air & Space Defense, 2020, 3(3): 83-88.
