The invention discloses a satellite shipborne communication-in-motion satellite-aligning semi-physical simulation method and system, and the method comprises the steps: carrying out the satellite ephemeris calculation and satellite trajectory prediction based on a sath toolbox and customized multivariate two-line report TLE data, and generating a target satellite for a satellite-aligning process of communication-in-motion; carrying out ship jolt simulation based on the sea wave power spectrum empirical function corrected by the sea area features, and adding disturbance to satellites for satellite communication in motion; performing simulation fitting on an actually measured inertial navigation data error model and a drift model based on the Airy variance, and feeding back a three-axis angle of the communication-in-moving antenna system in real time; based on cubic spline interpolation of a sensor error model and a drift model correction interpolation coefficient and multi-sensor synchronization of an extrapolation algorithm, simulation authenticity and data reliability are improved. The communication-in-motion semi-physical simulation platform established by the invention effectively restores the satellite communication process of the communication-in-motion antenna, ensures the stability of communication data input and output, supports introduction of actually measured data for semi-physical simulation, and verifies the accuracy of a satellite algorithm.

    本发明公开了一种卫星船载动中通对星半实物仿真方法及系统,所述方法包括基于satellite工具箱与自定义多元的两行报表TLE数据的卫星星历解算与卫星轨迹预测,为动中通对星过程生成目标卫星;基于海域特征修正的海浪功率谱经验函数,进行船舶颠簸模拟,为动中通对星添加扰动;基于艾伦方差的实测惯导数据误差模型与漂移模型的仿真拟合,实时反馈动中通天线系统三轴角度;基于传感器误差模型与漂移模型修正插值系数的三次样条插值、外推算法的多传感器同步,提高仿真真实性与数据可靠性。本发明搭建的动中通半实物仿真平台有效还原了动中通天线的对星通信过程,保证了通信数据输入输出的稳定性,支持引入实测数据进行半实物仿真,验证对星算法的准确性。


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    Titel :

    Satellite shipborne communication-in-motion satellite-to-satellite semi-physical simulation method and system


    Weitere Titelangaben:

    一种卫星船载动中通对星半实物仿真方法及系统


    Beteiligte:
    MA LI (Autor:in) / SUN QIANG (Autor:in) / ZHU RONGTAO (Autor:in) / JIANG XINGJIAN (Autor:in) / LEE HO-YEOP (Autor:in) / HUANG XUN (Autor:in) / YANG YONGJIE (Autor:in)

    Erscheinungsdatum :

    16.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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