THE THIRD ORDER SOLUTION OF ORBITAL PERTURBATION OF ARTIFICIAL EARTH'S SATELLITE

被引：0

作者：

刘林

赵德滋

机构：

[1] Department of Astronomy

[2] Nanjing University

来源：

Science China Mathematics | 1981年 / 06期

关键词：

perturbation; orbit; simpler; remaining; auxiliary; integrable; intuitive; constants; Delaunay; quantities;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

This paper gives a third order solution of orbital perturbation of artificial earth’s statel-lite on the basis of intermediate orbit, which is closed for eccentricity e. The method is con-venient to use and the solution is much simpler.

引用

页码：813 / 828

页数：16