编队飞行相对倾斜构形的 e／i矢量控制方法

摘要

The problem of relative inclined configuration design and orbit control of the distributed InSAR satellites formation flying was studied . First , the algorithm of relative inclined configuration design based on e/i vector was put forward . Then the relationship between the relative inclined configuration and the errors of eccentricity , inclination and the right ascension of ascending node were given . According to the properties of relative inclined configuration of distributed satellites , the four-impulse orbit maneuver strategy was put forward based on the Gauss perturbation functions satellite formation control model . Simulation results show that the method of relative inclined configuration design is intuitionistic , the orbit maneuver strategy is simple and the configuration is stable .%针对分布式卫星编队飞行相对倾斜构形设计与控制问题进行了研究，提出了基于e/i矢量相对运动模型的相对倾斜构形设计算法，给出了相对倾斜构形与偏心率偏差、轨道倾角偏差和升交点赤经偏差的关系，并针对相对倾斜构形偏置量的特点，提出了基于高斯摄动方程编队控制模型的一种四脉冲构形捕获控制算法，仿真结果表明，以 e/i矢量进行构形设计，方法直观，捕获控制策略简单，绕飞构形稳定。