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卫星动力学的英文

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"卫星动力学"怎么读用"卫星动力学"造句

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  • satellite dynamics

例句与用法

  • The main contributions are as follows : first , the early - warning with infrared cameras dynamics and kinematics equations are established
    本文主要研究内容如下:第一,建立了带有红外相机的预警卫星动力学方程,同时推导了运动学方程。
  • 4 . the three - axis attitude stabilization system of the flexible satellite has been studied , in which three basic vibration modes of the solar array have been considered
    4 、在挠性卫星动力学模型的基础上,建立了只考虑太阳帆板三阶振动模态的挠性卫星三轴姿态控制模型。
  • 5 . the dynamic system of the liquid - solid coupled satellite that is filled with an ideal liquid has been researched . the external disturbances and the liquid viscosity have been concerned in this study
    5 、针对带有椭球腔全充液的卫星,建立了液体做均匀涡旋运动的充液卫星动力学模型,分析了外界干扰和液体阻尼对卫星姿态稳定的影响。
  • High precision orbit propagation is the basis of the study of orbital dynamics , and the application of general engineering simulation platform , such as matrixx , matlab , will increase the efficiency and reliability of simulation
    卫星精密轨道预报是卫星动力学研究的基础,而成熟的通用工程仿真平台,如matrixx 、 matlab的应用将使仿真计算的效率与可靠性提高。
  • The main researches enclosed in this thesis are as follows : 1 . based on the newton ' s law of motion , the law of angular momentum and the variation principle , the dynamic model of the satellite with a flexible appendage has been researched
    主要内容有五个方面: 1 、运用牛顿定律、角动量定律和变分原理建立了带挠性附件的卫星动力学模型,分析了挠性太阳帆板转动对卫星动力学模型的影响。
  • In order to study small satellite attitude control system , the author first establishes the small satellite dynamics , kinematic models , and gives the theories of the quarternion , then study in - depth of the principles of the active magnetic control
    为研究主动磁控小卫星姿态控制系统,首先建立了主动磁控小卫星动力学、运动学模型,并给出了姿态四元数的相关理论。从地磁场模型出发,深入研究了主动磁控的原理。
  • The dynamic model of the satellite with a flexible appendage has been studied in this thesis . also , the techniques of the satellite earth acquisition and three - axis attitude stabilization of both the rigid satellite and the liquid - filled satellite have been researched
    本文针对单翼大挠性太阳帆板卫星,建立了挠性卫星动力学模型,在此基础上,研究了地球捕获、刚体卫星三轴姿态稳定、充液卫星三轴姿态稳定问题。
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