首页 | 本学科首页   官方微博 | 高级检索  
     检索      

对数螺旋线非开普勒轨道的可行性分析
引用本文:郑莉莉,袁建平,朱战霞.对数螺旋线非开普勒轨道的可行性分析[J].宇航学报,2010,31(1):31-35.
作者姓名:郑莉莉  袁建平  朱战霞
作者单位:西北工业大学航天学院,西安 710072
摘    要:提出了基于形状的非开普勒轨道设计方法,并分析了对数螺旋线轨道的应用可行性。 首先在假定轨道形状的前提下,通过变量代换推导出了在极坐标系下一般曲线用于轨道设计 的基本方程;然后分析了对数螺旋线表达式中的关键参数与航迹角的关系,得到了相应轨道 的基本性质;最后对待定参数的对数螺旋线轨道应用的可行性进行了推导和分析,结果显示 采用对数螺旋线设计非开普勒轨道是可行的,但仅适用于从椭圆初始轨道实现转移的情况。



关 键 词:非开普勒轨道  轨道设计  基于形状  对数螺旋线  可行性  
收稿时间:2009-10-12

Feasibility of the Logarithmic Spiral Non-Keplerian Orbit
ZHENG Li-li,YUAN Jian-ping,ZHU Zhan-xia.Feasibility of the Logarithmic Spiral Non-Keplerian Orbit[J].Journal of Astronautics,2010,31(1):31-35.
Authors:ZHENG Li-li  YUAN Jian-ping  ZHU Zhan-xia
Abstract:A new approach named shape-based non-Keplerian orbit design method was proposed. The intention of this paper is to analyze the feasibility of the logarithmic spiral orbit. First, the orbit shape was assumed with alterable parameter, under the circumstances, the general equation was presented according to variable transformation in which common curves could be utilized in orbit design with respect to polar coordinates. In addition, essential characteristics of the logarithmic spiral were developed by means of analyzing the relation between the key parameter and flight angle. In the end, the feasibility of non-Keplerian orbit design based on logarithmic spiral was derived and elucidated. The analysis results demonstrate that the application of the logarithmic spiral is feasible in the condition of the initial ellipse orbit.
Keywords:Non-Keplerian orbit  Orbit design  Shape-based method  Logarithmic spiral  Feasibility
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号