Taking the long-range air-to-air missile as the research object, this paper puts forward an angle-constrained range-extending trajectory planning scheme. Then, aiming at the problem of trajectory design in different flight segments, a kind of overload control climbing range-extended guidance law considering the current speed of missiles is studied, and the molding guidance law satisfying the terminal position and incident angle constraints based on optimal control theory is studied. The simulation results show that under typical launch conditions, the range of the proposed angle-constrained range-extended trajectory and its composite guidance laws can be increased by more than 20% compared with conventional trajectory and their guidance laws, and can meet the constraints of line of sight angle and incident angle.


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    Titel :

    Research on Long-Range Air-to-Air Missile Extended Range Trajectory Guidance Law with Angle Constraint




    Erscheinungsdatum :

    2022




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt





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