Study on interception control strategies with zero effort miss

摘要

In the present paper the terminal orbital control in the satellite pursuit-evasion game was studied, where the orbital maneuver with using limited magnitude continuous thrust was involved for both the interceptor and target. Since considering the terminal application scenario the high nonlinear interception dynamics could be reduced to the CW equations. Based on the reduced CW equation, zero effort miss was proposed to obtain the orbit control strategy. And with adding the fuel consumption the controller was built. Finally, the proposed method was validated by the numerical simulation, and the advantage and weakness of the proposed control strategy was analyzed.