• 文章分析卫星轨道热流平均温度周期分布温度进行实时预测。

    In this paper, satellites temperature is predicted on-line after the analysis to the cycles of orbital external thermal current and average temper a ture.

    youdao

  • 速度各分量变化具有很明显周期卫星轨道的运行周期相吻合

    The variations of velocity difference have obvious periodicity, which coincides with the satellite orbit period.

    youdao

  • 对话框左边目录显示了当前数据文件中的卫星名称及其分钟计算轨道周期

    The list on the left side of the dialog shows the names of all the objects in the current data file, together with each object's orbital period in minutes.

    youdao

  • 观测卫星轨道具有全球目标覆盖太阳同步特性通过设计轨道周期轨道倾角可以获得这些特性

    Global coverage and sun synchronization are the essential properties of the earth observation satellites, which are assumed by designing the orbit period and inclination.

    youdao

  • 编队卫星相对距离较大非线性因素不可忽略利用非线性周期运动条件,找到不需消耗任何燃料的周期性相对运动轨道

    When the relative range was large and the effects of nonlinearity could not be neglected, the nonlinearity periodic relative rotating orbits could be found using the nonlinearity initial conditions.

    youdao

  • 极地上工作的对地定向卫星动力学方程一个线性周期系统

    The magnetic control system for polar orbiting, nadir pointing small satellite is studied in this paper. It is shown that the dynamics with magnetic control system is a linear periodic system.

    youdao

  • 由于磁场方向轨道周期变化卫星姿态动力学方程一个线性周期系统

    Since the geomagnetic field varies periodically on orbit, the dynamics of satellite is a linear periodic system.

    youdao

  • MEOIGSO卫星一个轨道周期内星历参数拟合结果变化规律相近,但是GEO卫星差异较大。

    It also shows that the variety laws of the fitting result of broadcast ephemeris for MEO and IGSO satellites are similar to each other and are different to GEO satellites.

    youdao

  • 电动力卫星的推力幅值较小且方向固定,完成轨道机动任务周期长,控制问题的求解比较困难。

    Electrodynamic tethers with low thrust-to-weight ratios can only perform orbital transfers over a large number of revolutions, which poses a real challenge to short time scale optimal control methods.

    youdao

  • 电动力卫星的推力幅值较小且方向固定,完成轨道机动任务周期长,控制问题的求解比较困难。

    Electrodynamic tethers with low thrust-to-weight ratios can only perform orbital transfers over a large number of revolutions, which poses a real challenge to short time scale optimal control methods.

    youdao

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