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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)
