纳米卫星定位与稳定方法分析

2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Pub Date : 2016-10-01 DOI:10.1109/MSNMC.2016.7783131

V. Yavisya, N. M. Bendasiuk

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引用次数: 6

摘要

研究了超小型航天器空间位置的定位与稳定方法。传统的定向和稳定方法是根据其可行性来衡量的，考虑到对重量和总体性能的限制，与能源消耗相关的操作限制以及轨道变化的可能性。

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Analysis of methods for orientation and stabilization of nano-satellites

Paper deals with methods of orientation and stabilization of the spatial position of the ultra-small spacecraft. Traditional methods of orientation and stabilization are measured in terms of their feasibility, taking into account the restrictions on weight and overall performance, operational constraints associated with energy consumption, as well as the possibility of orbit changing.

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来源期刊

2016 4th International Conference on Methods and Systems of Navigation and Motion Control (MSNMC)

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