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在卫星编队飞行相对运动方程的基础上提出了一种基于最小二乘估计的卫星编队飞行轨道设计方法,即在参考卫星轨道根数、相对运动轨迹和伴随卫星近点幅角已知的情况下应用最小二乘估计法设计伴随卫星其余轨道根数。该方法不仅能够应用于小偏心率参考轨道情况下的相对轨道设计,而且能够解决大偏心率参考轨道情况下的相对轨道设计问题。仿真结果表明该方法可行。
Based on the relative motion equation of satellite formation flight, a method of designing satellite formation flight path based on least squares estimation is proposed. That is to say, when the number of reference orbit, the relative motion trajectory and the argument of the satellite near point are known The least square estimation method is used to design the number of the remaining orbits of the satellite. This method not only can be applied to the relative orbit design in the case of small eccentricity reference track, but also can solve the relative orbit design problem in the case of large eccentricity reference track. Simulation results show that this method is feasible.