文件名称:gauss
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利用高斯迭代法，求解二体问题航天器状态向量。-This function uses the Gauss method with iterative improvement
(Algorithms 5.5 and 5.6) to calculate the state vector of an orbiting body angles-only observations at three closely-spaced times.
(Algorithms 5.5 and 5.6) to calculate the state vector of an orbiting body angles-only observations at three closely-spaced times.
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gauss.m
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