首页> 外国专利> METHOD FOR CONTROLLING THE PITCH ATTITUDE OF A SATELLITE BY MEANS OF SOLAR RADIATION PRESSURE, AND A SATELLITE, FOR IMPLEMENTING SAME

METHOD FOR CONTROLLING THE PITCH ATTITUDE OF A SATELLITE BY MEANS OF SOLAR RADIATION PRESSURE, AND A SATELLITE, FOR IMPLEMENTING SAME

机译:通过太阳辐射压力来控制卫星俯仰姿态的方法和一种实现相同目标的卫星

摘要

A satellite comprises at least one surface (4, 5) intended mainly for exposure to solar radiation and extending away from the satellite in a predetermined direction (Y), an on-board computer (8) having connected thereto an attitude sensing system (7), an orbit control system for imparting thrust to the satellite along predetermined axes, and an attitude control system. Said satellite further comprises a device (6') for controlling the tilt of said surface in parallel with a plurality of planes containing said predetermined direction (and therefore particularly in parallel with the plane of a solar panel forming said surface). Said tilt control device is controlled by said on-board computer. Said tilting can generate a moment of pitch or relocate the centre of gravity onto the axis of the orbit control system.
机译:卫星包括至少一个主要用于暴露于太阳辐射并在预定方向(Y)上远离卫星延伸的表面(4、5),以及与姿态感测系统(7)连接的车载计算机(8)。 ),用于沿预定轴向卫星施加推力的轨道控制系统和姿态控制系统。所述卫星还包括用于控制所述表面的倾斜度的装置(6'),所述倾斜度与包含所述预定方向的多个平面平行(并且因此特别是平行于形成所述表面的太阳能电池板的平面)。所述倾斜控制装置由所述车载计算机控制。所述倾斜可产生俯仰力矩或将重心重新定位在轨道控制系统的轴线上。

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