Attitude control operations on rkoreasat satellites

机译：rkoreasat卫星的姿态控制操作

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This paper dsicusses the effective attitue control operation of Koreasat satellits under normal operation mode and during stationkeeping maneuvers through the analysis of the effects of solar presure disturbances, the thruster plume impingement, the charadteristics of MATS(Momentum Alignment Trim Selectron) and APEMAC(Automatic Pitch Error/Momentum Adjust Control) operations.

机译：本文通过分析太阳压力干扰，推进器羽流撞击，MATS（动量对准饰面Selectron）和APEMAC（自动俯仰）的特性，分析了大卫星卫星在正常工作模式和驻地演习期间的有效服装控制操作。错误/动量调整控件）操作。

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来源
《4th IFAC(International Federation of Automatic Control) Symposium on Automatic Control in Aerospace 1998 Seoul, Korea, 24-28 August 1998》|1998年|p.289-293|共5页
会议地点 Seoul(KR)
作者
Han Hwangbo; Changpyo Oh; Yongioong Yoon;
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原文格式 PDF
正文语种 eng
中图分类航空、航天技术的研究与探索;
关键词
Kroeasat attitude control operation; disturbance torque; stationkeepting; plume disturbance;

机译：Kroeasat姿态控制操作；扰动扭矩守财奴;羽状扰动;

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机译：RKOREASAT卫星的态度控制操作
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Attitude control operations on rkoreasat satellites

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