王大轶1, 侯博文1,2, 王炯琦2, 葛东明1, 李茂登3, 徐超3, 周海银2
CJA
收稿日期:2020-05-28
修回日期:2020-06-16
发布日期:2020-07-06
通讯作者:
侯博文
E-mail:houbowen95@126.com
基金资助:WANG Dayi1, HOU Bowen1,2, WANG Jiongqi2, GE Dongming1, LI Maodeng3, XU Chao3, ZHOU Haiyin2
Received:2020-05-28
Revised:2020-06-16
Published:2020-07-06
Supported by:摘要： 自主导航是航天器自主运行的核心关键技术。状态估计是实现航天器自主导航的核心手段，是指实时确定航天器在轨位置、速度和姿态等导航参数，是航天器自主导航技术的重点发展方向之一。首先，针对航天器自主导航的实际需求，阐述了研究航天器自主导航状态估计方法的必要性，具体从导航系统可观测性分析、导航滤波算法、导航系统误差补偿3个方面介绍了航天器自主导航状态估计方法的研究现状；然后，分析并总结状态估计方法在航天器自主导航系统中的实际应用；最后，结合理论研究和实际应用，给出了状态估计方法目前存在的主要问题并对其后续发展进行了展望。
中图分类号:
王大轶, 侯博文, 王炯琦, 葛东明, 李茂登, 徐超, 周海银. 航天器自主导航状态估计方法研究综述[J]. 航空学报, 2021, 42(4): 524310-524310.
WANG Dayi, HOU Bowen, WANG Jiongqi, GE Dongming, LI Maodeng, XU Chao, ZHOU Haiyin. State estimation method for spacecraft autonomous navigation: Review[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524310-524310.
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