Abstract

Problems on optimizing the noncoplanar flights with low thrust from elliptical to geosynchronous orbits for different control accelerations are solved. Recommendations for choosing an initial approximation are given. The results are compared with the results obtained by other authors.

中文翻译：

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低推力非共面飞行的线性化方法

摘要

解决了针对不同的控制加速度，优化从椭圆轨道到地球同步轨道的低推力非共面飞行的问题。给出了选择初始近似值的建议。将结果与其他作者获得的结果进行比较。