The invention discloses a helicopter satellite communication anti-rotor wing shielding key technology research method. The method comprises the following steps S01, enabling a sending terminal to divide a sending source code into a plurality of continuously arranged data segments; S02, performing dual time diversity on the modulated data segment; S03, establishing satellite communication channel models of the sending end and the receiving end; S04; combining the data segments after diversity and carrying out diversity, and sending the data segments through a communication channel model; and S05, enabling a receiving terminal to receive a code element, and acquiring a shielding time value of each rotor shielding period. In the present invention, according to the helicopter satellite communication anti-rotor wing shielding research method, a dual time diversity technology is adopted; the shielding time period value of the helicopter rotor wing on the satellite communication system duringdata communication can be detected, and the shielding influence of the helicopter rotor wing on the communication data in the satellite communication system is avoided, so that fading of the satellite communication data and loss of the data are avoided, and the accurate and complete communication quality of the helicopter satellite communication system is ensured.

    本发明公开了直升机卫星通信抗旋翼遮挡关键技术研究方法,包括以下步骤:S01:发送端将发送源码分割成多个连续排列的数据段;S02:对调制后的数据段进行双重时间分集;S03:建立发送端与接收端的卫星通信信道模型;S04;将分集后的数据段合并分集后通过通信信道模型发送;S05:接收端接收码元,获取每个旋翼遮挡周期的遮挡时间值。本发明中,该直升机卫星通信抗旋翼遮挡研究方法采用双重时间分集的技术,可以检测到直升机旋翼对卫星通信系统数据通信时的遮挡时间周期值,避免了直升机的旋翼对卫星通信系统内通信数据的遮挡影响,从而避免了卫星通信数据的衰落和数据的丢失,确保了直升机卫星通信系统准确、完整的通信质量。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Helicopter satellite communication anti-rotor wing shielding key technology research method


    Weitere Titelangaben:

    直升机卫星通信抗旋翼遮挡关键技术研究方法


    Beteiligte:
    LI ZHIQIANG (Autor:in)

    Erscheinungsdatum :

    13.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    Helicopter rotor wing wingtip lamp

    XING ZHIZHEN / HE MIN / DI ZHAO | Europäisches Patentamt | 2025

    Freier Zugriff

    Rotor wing operating system of coaxial double-rotor-wing helicopter

    WU JIREN / WU JING | Europäisches Patentamt | 2024

    Freier Zugriff

    Helicopter tail rotor wing with detachable structure and production process of helicopter tail rotor wing

    YAO ERQIANG / ZHU XUAN / CHU PENGFEI et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Helicopter rotor wing control universal joint

    WU SHANG | Europäisches Patentamt | 2024

    Freier Zugriff

    Rotor wing speed reducer and helicopter

    ZHAO NING / DU MINBO | Europäisches Patentamt | 2025

    Freier Zugriff