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  • The variation equation of the satellite orbit elements under both J2 and drag perturbations was derived based on the Gauss perturbation equation.

    基于高斯摄动方程，推导了卫星在同时考虑J2和大气摄动情况下的轨道根数变化方程。

    youdao

  • The variation equation of the satellite orbit elements under both J2 and drag perturbations was derived based on the Gauss perturbation equation.

    基于高斯摄动方程，推导了卫星在同时考虑J2和大气摄动情况下的轨道根数变化方程。

    youdao

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