CAJ | 학술논문

根据编队合成孔径雷达干涉（InSAR）卫星的轨道特点和星间紧密编队的特性,引入e/i矢量概念,推导了用e/i矢量表示的编队卫星相对运动学方程,分析了在满足测量基线条件和星间距离条件下编队构型设计约束,并给出了能实现全球测量的编队构型设计结果。对获得的编队飞行轨道参数的数学仿真结果表明：设计的编队构型正确。
근거편대합성공경뢰체간섭（InSAR）위성적궤도특점화성간긴밀편대적특성,인입e/i시량개념,추도료용e/i시량표시적편대위성상대운동학방정,분석료재만족측량기선조건화성간거리조건하편대구형설계약속,병급출료능실현전구측량적편대구형설계결과。대획득적편대비행궤도삼수적수학방진결과표명：설계적편대구형정학。
To get orbit elements from the relative position of two satellites,e/i vector method was proposed according the characteristics of the orbit for InSAR and close forming flying in this paper.The relative motion equation was deduced using e/i vector method.The design of formation flying shape which the conditions of the baseline and relative distance between satellites were met was analyzed,and design results of the formation flying shape which could realize the globule survey were acquired.The simulation results with the formation flying orbit elements acquired showed that the formation flying designed was correct.