Compound Cooperative Guidance for High Parabolic Trajectory in Three-Dimensional Space

Abstract

Cooperative guidance problem of multiple missile system in three-dimensional space is investigated in this paper. Guidance commands in pitch plane and lateral plane of initial guidance, mid-course guidance and terminal guidance are designed, and the rules of shift guidance in different guidance stages are given.The numerical simulation results of high parabolic trajectory are given in two cases, and the performance characteristics of the compound cooperative guidance law are obtained. The effectiveness of the theoretical method proposed in this paper is verified, which provides a possible solution to the problem of multi-missile cooperative attack.

Keywords

• |missile guidance|high parabolic trajectory|cooperative guidance|impact time constraint|compound guidance