共面编队飞行卫星星座的控制

共面编队飞行的卫星星座的相对运动轨迹是一个椭圆,但卫星由于受摄动力的影响,其椭圆队形会发生变化。提出了一个简单而又节约燃料的队形保持控制方案,即在Hill轨道坐标系中,通过测量x轴和z轴,利用小推力喷气发动机进行控制,消除椭圆中心的相位漂移和各卫星轨道的不共面。

The Control of the Satellites Coplanar Formation Flying

The figure of the relative kinematical track of the formation flying will change which is in an ellipse because of the disturbing force from which the satellites suffer. A simple way of control is developed that saves the fuel, that is, in Hill orbital coordinates, through the measurement of x-axis and z-axis, the control of the small jet engine will eliminate the phase excursion of the center of the ellipse and the non-coplanarity of the orbit of satellites.