The present invention discloses a recovery control method and apparatus for a rocket, an electronic device and a storage medium. The recovery control method for a robot comprises: acquiring an airflow angle of attack and an airflow angle of sideslip, and calculating an aerodynamic force according to the airflow angle of attack and the airflow angle of sideslip; acquiring a mass and an engine thrust of the rocket; and determining a standard reference trajectory of the rocket by using the aerodynamic force, the engine thrust and the mass. That is to say, by adding statistics of change rules of a wind field in a design process of a rocket returning and landing ballistic trajectory, a flight ballistic trajectory design value during a return process is closer to a real flight state, thereby ensuring that a guidance control method is more effective during the return process, and ensuring a greater probability of safe return of the recovered rocket to a landing site.


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    Titel :

    RECOVERY CONTROL METHOD AND APPARATUS FOR ROCKET, ELECTRONIC DEVICE AND STORAGE MEDIUM


    Weitere Titelangaben:

    VERFAHREN UND VORRICHTUNG ZUR STEUERUNG DER WIEDERHERSTELLUNG EINER RAKETE, ELEKTRONISCHE VORRICHTUNG UND SPEICHERMEDIUM
    PROCÉDÉ DE COMMANDE DE RÉCUPÉRATION ET APPAREIL POUR FUSÉE, DISPOSITIF ÉLECTRONIQUE ET SUPPORT DE STOCKAGE


    Beteiligte:
    PENG XIAOBO (Autor:in) / ZHENG LIWEI (Autor:in) / SHI JIANBO (Autor:in)

    Erscheinungsdatum :

    2023-09-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64G Raumfahrt , COSMONAUTICS



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