本文選題：傾斜軌道　切入點(diǎn)：太陽高度角　出處：《空間控制技術(shù)與應(yīng)用》2016年03期 　論文類型：期刊論文

【摘要】：針對傾斜軌道小衛(wèi)星必然會面對的光學(xué)姿態(tài)敏感器受陽光干擾的問題,分析太陽高度角的變化規(guī)律,提出了計(jì)算太陽高度角的經(jīng)驗(yàn)公式,并在此基礎(chǔ)上提出了平臺偏航姿態(tài)機(jī)動方案,可以使光學(xué)姿態(tài)敏感器規(guī)避陽光干擾,并可以簡化整星熱控和帆板驅(qū)動設(shè)計(jì),提高了整星的可靠性.
[Abstract]:In view of the problem that the optical attitude sensor will be disturbed by the sun, the variation law of the solar altitude angle is analyzed, and the empirical formula for calculating the solar altitude angle is put forward. On this basis, a platform yaw attitude maneuver scheme is proposed, which can make the optical attitude sensor avoid the sun interference, simplify the whole satellite thermal control and the design of the board driving, and improve the reliability of the whole satellite.
【作者單位】： 上海航天控制技術(shù)研究所;上海市空間智能控制技術(shù)重點(diǎn)實(shí)驗(yàn)室;上海航天技術(shù)研究院;
【基金】：上海航天核攀資助項(xiàng)目(ZY2015-003-3)
【分類號】：V448.2
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本文編號：1569617