摘要
针对导航卫星中轨道(MEO)轨道提出一种上面级发射MEO轨道直接入轨设计方案,建立轨道动力学方程和轨道迭代计算模型。为优化轨道设计,将更多有效载荷送入轨道,从分析影响轨道运载能力的因素出发,应用成熟优化算法——自适应遗传算法,建立上面级发射MEO轨道优化模型,采用数值仿真方法验证设计结果和优化方法的有效性。结果表明发射轨道优化设计对运载能力有一定的提升效果,实现了最优化设计。
Based on the analysis of the MEO(Medium Earth Orbit)orbit for navigation satellites,a design method of MEO lunching direct injection with upper stage is proposed,and orbital dynamic equation and iterative calculations model are built.For sending more payloads into orbit,the key factors that affect launching capability are analyzed,and the objective optimization model based on adaptive genetic algorithm is established for optimizing launching trajectory.A numerical simulation proves the validity of the design method and optimization method.The result shows that the optimization method is favorable for increasing launching capability.
作者
王传魁
焉彬
张利宾
郑莉莉
陈佳晔
周文勇
陈益
WANG Chuankui;YAN Bin;ZHANG Libin;ZHENG Lili;CHEN Jiaye;ZHOU Wenyong;CHEN Yi(Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China)
出处
《宇航总体技术》
2020年第6期44-49,共6页
Astronautical Systems Engineering Technology
基金
航天系统部专用技术(30506050301)
关键词
上面级
MEO轨道
直接入轨
轨道优化
Upper stage
MEO orbit
Directly injecting mode
Trajectory optimization
