Publication Date:
2019-06-27
Description:
Equations were derived for the perturbations on an artificial satellite when the motion of the satellite is commensurable with that of the earth. This was done by first selecting the tesseral harmonics that contribute the most to the perturbations and then by applying Hori's method by use of Lie series. Here, are introduced some modifications to the perturbations, which now result in better agreement with numerical integration.
Keywords:
ASTRODYNAMICS
Type:
NASA-CR-146854
,
SAO-SPECIAL-REPT-373-PT-2
Format:
application/pdf