卫星初始模式定位的制导和经济数字控制

2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI:10.23919/ICINS.2018.8405936

T. Somova

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引用次数: 2

摘要

本文提出了一种信息卫星初始模式下的经济数字姿态控制算法:从卫星与发射火箭分离到轨道参照系的常规姿态稳定。讨论了太阳同步轨道上陆地测量卫星初始定位模式的计算机仿真结果。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Guidance and economical digital control of a satellite orientation in initial modes

The paper presents the algorithms for economical digital attitude control of an information satellite at initial modes: from the time it separates from a launcher rocket up to its regular attitude stabilization in the orbital reference frame. The computer simulation results on the initial orientation modes of a land-survey satellite on a sun-synchronous orbit are discussed.

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来源期刊

2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)

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