It is very difficult to conduct time cooperation guidance of multi-missile when the velocity of missile is uncontrollable. Based on the trajectory super real-time simulation method, which can gives out time-to-go exactly as well as future trajectory information, a closed-loop control system between the horizontal control overload and the flight time error of missiles is built. So that the flight time tends to be consistent and the cooperative impact time is realized. In addition, a trajectory shaping guidance law with impact angle constraints is designed. The designed guidance law is verified by 6-DOF simulation, and the results show that the multi-missile cooperative guidance law based on the super real-time trajectory simulation can guarantee that multi-missile hit the target with the desired impact angle simutaneously.


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    Titel :

    Research on Cooperative Guidance Law of Multi-Missile Based on Trajectory Super-Real Time Simulation


    Beteiligte:


    Erscheinungsdatum :

    2021




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




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