搜索资源列表
guidao
- 卫星在已知轨道六根数的情况下,需要求得其位置速度时的转换软件,非常方便。是基于兰波特方法计算的
EXERCISE_3_3
- 计算特定卫星轨道选择合适的力学模型,评估卫星上各种摄动力-Calculate specific satellite orbital mechanics to choose the right model, the assessment of a variety of satellite perturbation
ECI_ECEF
- ECI与ECEF转换关系,卫星轨道模型方法,应用相关(ECI and ECEF conversion relation, satellite orbit model method, application correlation)
J2
- 考虑地球扁率摄动,求解近地卫星轨道六根数,(Consider J2 perturbation to solve the number of six tracks)
