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以电磁编队飞行动力学为研究对象,建立基于地心惯性坐标系的电磁编队动力学方程,推导出相对轨道动力学模型.考虑到工作姿态对于编队卫星工作的重要性,对基于反应轮调整卫星姿态的姿态动力学方程也进行了公式推导.该工作可以为后续的电磁编队控制方案及其仿真的研究工作提供必要的理论基础.
Taking electromagnetic formation flight dynamics as the research object, the electromagnetic formation dynamics equation based on the geocentric inertial coordinate system is established, and the relative orbit dynamics model is derived. Taking into account the importance of the working attitude for the formation satellite, Attitude attitude dynamics equations have also been derived formulary.This work can provide the necessary theoretical basis for the follow-up study of electromagnetic formation control program and its simulation.