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THE THIRD ORDER SOLUTION OF ORBITAL PERTURBATION OF ARTIFICIAL EARTH’S SATELLITE
【摘要】 <正> 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.
【Abstract】 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.
【关键词】 perturbation；
orbit；
simpler；
remaining；
auxiliary；
integrable；
intuitive；
constants；
Delaunay；
quantities；
- 【文献出处】 Science in China,Ser.A ,中国科学A辑(英文版) , 编辑部邮箱 ,1981年06期
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