A launch planning method for airborne missile defence guidance comprising the steps of calculating flight trajectory of an incoming missile from the current time to the moment of hitting a carrier aircraft, based on the current motion state of the incoming missile and the carrier aircraft and then establishing an interceptor missile group formation with interception feasibility through reachable set analysis and coverage strategy based on the calculated flight trajectory of the incoming missile The interceptor missile group formation is obtained at different time nodes, calculating the time and angle constraints in the flight of the guidance formation in three dimensions, and determining the interceptor missile group formation and the launch timing of each missile. The interceptors are launched to achieve group formation through mid-course guidance, and each interceptor reaches the corresponding position in the formation at the same time with the desired formation time and velocity vector, forming an interceptor formation against the incoming missile, and then intercepting the incoming missiles through cooperative terminal guidance.


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    Title :

    A launch planning method for airborne missle defence guidance


    Publication date :

    2023-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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