Distributed adaptive cooperative guidance for multi-missile salvo attack
Zou Li1, Kong Fane2, Zhou Rui3, Wu Jiang3*
1. Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;
2. Key Laboratory of National Defense on Fire Control Technology, Luoyang Institute of Electro-optical Equipment, Luoyang 471009, China;
3. Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
A distributed adaptive cooperative guidance law for multi-missiles with heterogeneous leader-follower was proposed to implement salvo cooperative attacks. On the basis of local communication and traditional proportional guidance law, a distributed cooperative guidance law for multiple heterogeneous missiles with leader-follower was developed using the principles of synchronization in coupled dynamic networks. The distributed cooperative guidance of the leader missile was based on the proportional navigation guidance law with constant navigation coefficient, while the distributed cooperative guidance of the follower missile was based on the proportional guidance law with adaptive variable navigation coefficient. The effectiveness of the proposed distributed adaptive cooperative guidance law was demonstrated by the simulation results of five missiles salvo attacks.