The invention relates to a propeller unmanned aerial vehicle in-box launching simulation method. The launching process in the propeller unmanned aerial vehicle box is divided into four stages, respectively, an in-box sliding stage, an air rocket boosting stage, an unpowered gliding stage and a propeller acting stage. The six-degree-of-freedom model of the propeller unmanned aerial vehicle in eachstage in the launching process is obtained. A simulation method is provided for calculating information such as the posture, the height and the speed of the unmanned aerial vehicle in the launching process.

    本发明涉及一种螺旋桨无人机箱内发射仿真方法,将螺旋桨无人机箱内发射过程分为四个阶段,分别为箱内滑行阶段、空中火箭助推阶段、无动力滑翔阶段和螺旋桨作用阶段,得到螺旋桨无人机在发射过程中每个阶段的六自由度模型,为计算无人机在发射过程中姿态、高度、速度等信息提供了一种仿真方法。


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    Titel :

    Propeller unmanned aerial vehicle in-box launching simulation method


    Weitere Titelangaben:

    一种螺旋桨无人机箱内发射仿真方法


    Beteiligte:
    AN BIN (Autor:in) / YANG JUNPENG (Autor:in) / MENG MAOMAO (Autor:in) / LI BO (Autor:in)

    Erscheinungsdatum :

    02.10.2020


    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



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