Design of Multi-Missile Cooperative Guidance Law Based on Pulse Engine Characteristics

• Published in: Hangkong Bingqi Vol. 29; no. 1; pp. 41 - 46
• Main Author: Pan Hui, Zhang Zhenlin, Guo Chao
• Format: Journal Article
• Language: Chinese
• Published: Editorial Office of Aero Weaponry 01.02.2022
• Subjects: cooperative guidance|consistency theory|angle constraint|impulse engine characteristics|sliding mode variable structure control|discrete guidance|missile
• DOI: 10.12132/ISSN.1673-5048.2021.0069
• ISSN: 1673-5048

Aiming at the design problem of multi-missile cooperative guidance law for attacking high-speed targets, a design method of multi-missile cooperative guidance law based on the working characteristics of pulse engine is proposed. Firstly, the relative motion equation of missile and target is solved. Secondly, the finite-time consistency theory is used to design the cooperative guidance law in the line-of-sight direction, and the sliding mode variable structure control theory is used to design the line-of-sight angle constrained guidance law in the line-of-sight normal direction. Then, for the overload command in the line-of-sight direction, considering the working characteristics of the pulse engine, the continuous guidance command in the line-of-sight system is transformed into discrete guidance command, and then the multi-missile cooperative guidance is realized. Finally, the feasibility and effectiveness of the designed multi-missile cooperative guidance law are verified by numerical simulation.