CAJ | 학술논문

基于共椭圆轨道接近策略，航天器交会轨迹基本上可分为5类：共椭圆视线推力逼近；V—bar稳定轨道点逼近；双共椭圆轨道逼近；共椭圆加偏置点逼近；稳定轨道与共椭圆组合逼近。给出包括“双子座”、“阿波罗”、航天飞机、“联盟”号和“进步”号、“自动转移飞行器”（ATV）、“H-Ⅱ转移飞行器”（HTV）、神舟八号，以及“猎户座”、“龙”、“天鹅座”等追踪航天器的各种交会轨迹图，分析各类交会轨迹的特点，可供交会对接任务设计选择与应用。
기우공타원궤도접근책략，항천기교회궤적기본상가분위5류：공타원시선추력핍근；V—bar은정궤도점핍근；쌍공타원궤도핍근；공타원가편치점핍근；은정궤도여공타원조합핍근。급출포괄“쌍자좌”、“아파라”、항천비궤、“련맹”호화“진보”호、“자동전이비행기”（ATV）、“H-Ⅱ전이비행기”（HTV）、신주팔호，이급“작호좌”、“룡”、“천아좌”등추종항천기적각충교회궤적도，분석각류교회궤적적특점，가공교회대접임무설계선택여응용。
Based on co-elliptic orbit proximity strategy, rendezvous and docking trajectories of spacecraft basically can be divided into five categories： co-elliptic orbit using thrust of line-of-sight, stable orbit point on V-bar, double co- elliptic orbits, co-elliptic orbit plus offset point, stable orbit point combined with co-elliptic orbit. Patterns of rendezvous trajectories of each chasing spacecraft, such as Gemini, Apollo, Space Shuttle, Soyuz and Progress, Automated Transfer Vehicle （ATV）, H-Ⅱ Transfer Vehicle （HTV）, Shenzhou VIII, as well as Orion, Dragon, Cygnus, etc. are presented, with their features analyzed, which can be useful to rendezvous mission designs.