A Method of Determining Multiple-targets Interception Based On Traversing Points

Space attack-defense confrontation is the commanding height in modern warfare. This paper takes space platform as research object and tries to solve problems such as space non-coplanar, large energy consumption of multiple-targets orbit interception and long interception time. Firstly, a design energy-optimal method of orbit interception based on Traversing Points is proposed. Secondly, the optimal design model of orbital interception is established. Finally, we take space platform interception of three targets in low earth orbit as an example and STK simulations' analysis is carried out to verify the effectiveness of the proposed method. The research provides a theoretical basis for analysing non-coplanar and multi-targets interception strategy.