Decentralized determination of relative orbit for formation flying satellite

D. Xue, Xibin Cao, Yunhua Wu
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引用次数: 10

Abstract

Autonomous formation flying is an important technology for the future space missions involving multiple satellites, and one of the key requirements of formation flying is accurate relative navigation. This paper develops an efficient approach of autonomous relative orbit determination for formation flying satellite. In view of that some formation flying satellites work at the orbits which are beyond the range of a GPS signal, inter-satellite measurements by the devices onboard the satellite instead of GPS measurements are chosen to perform this relative navigation. Several estimator architectures and associated algorithms are presented, among which the decentralized architecture is chosen because it can reduce the computational load as well as the communication requirements among the satellites, accordingly the orbit states estimation is achieved through a decentralized Schmidt-Kalman filter design. The simulation results verify the validity of this navigation method
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编队飞行卫星相对轨道的分散确定
自主编队飞行是未来多星空间任务的一项重要技术,而精确相对导航是编队飞行的关键要求之一。提出了一种有效的编队飞行卫星自主相对定轨方法。鉴于一些编队飞行卫星在GPS信号范围之外的轨道上工作,因此选择由卫星上的设备进行星间测量而不是GPS测量来进行这种相对导航。提出了几种估计器结构和相关算法,其中选择分散式结构,因为它可以减少计算量和卫星之间的通信需求,因此通过分散的施密特-卡尔曼滤波器设计实现轨道状态估计。仿真结果验证了该导航方法的有效性
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