摘要
针对载人航天任务中面临的与空间站保持长期共轨飞行的轨道问题,分析了航天器在地球扁率J_2项摄动以及大气阻力摄动作用下,长期共轨飞行航天器半长轴、相位和升交点赤经的变化特性,并设计了仅通过面内调整同时实现面内和面外调整的共轨维持的控制策略。通过仿真算例验证了控制策略的有效性,轨道维持的燃料消耗合理。可为我国载人航天器与空间站共轨方案设计提供参考。
Aiming at the orbital maintenance problem of keeping company with space station orbit for a long duration, the characteristics of semi-axis, phase and ascending node right ascension under the influence of J 2 perturbation and atmospheric drag are analyzed,and an orbital maintenance strategy of through plane maneuvering to realize plane and out-of-plane maintenance are proposed and simulated. Simulation results show that the orbital maintenance strategy and fuel consumption is reasonable. This paper can provide a reference for co-orbital manned-spacecraft and space station.
作者
刘欢
张柏楠
张永
LIU Huan;ZHANG Bainan;ZHANG Yong(Institute of Manned Space System Engineering,China Academy of Space Technology, Beijing 100094, China)
出处
《航天器工程》
CSCD
北大核心
2019年第2期19-23,共5页
Spacecraft Engineering
关键词
载人航天器
空间站
共轨轨道
地球非球形摄动
大气阻力
轨道维持
manned-spacecraft
space station
accompanying orbit
spherical earth gravitational perturbation
atmospheric drag
orbital maintenance
