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spacecraft orbit calculate

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你好 外推步长设置过大会出现nan 如sat.Propagate(3000,3000) 是否我缺少某一步关键计算 因为我有个需求,外推几年不考虑风阻

control strategy for GTO to GEO transfer

enhancement
good first issue

gound traj control for LEO Repeat Orbit

您好,请我下载下来的matlab压缩包是没有月心惯性系到月固系的转换函数吗?不怎么懂C++,请问是怎么转换的呢,我记得JPL星历表好像是8天时间内共用一组天平动数据,这样转换的话会不会精度不太够呢?

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