陈冰1, 郑勇1, 陈张雷1, 章后甜1,2, 刘新江1,3
收稿日期:
2019-11-27
修回日期:
2019-12-22
出版日期:
2020-08-15
发布日期:
2020-01-16
通讯作者:
陈冰
E-mail:ernestking@163.com
基金资助:
CHEN Bing1, ZHENG Yong1, CHEN Zhanglei1, ZHANG Houtian1,2, LIU Xinjiang1,3
Received:
2019-11-27
Revised:
2019-12-22
Online:
2020-08-15
Published:
2020-01-16
Supported by:
摘要: 临近空间是航天与航空业务领域的结合部,具有重要的战略价值。高超声速飞行器是临近空间力量部署的重要载体,已逐渐进入应用部署阶段。临近空间高超声速飞行器的飞行环境和任务条件对导航系统提出了新的更高要求。在总结临近空间高超声速飞行器的导航技术研究进展的基础上,对天文导航技术的应用环境和条件进行了系统的分析和探讨,提出了5个重点研究方向,包括:星图采集效能、光学误差模型、视场观测机理、姿态更新速率、小型化模块化工程化等。研究结果可为临近空间高超声速飞行器天文导航系统的设计提供参考。
中图分类号:
陈冰, 郑勇, 陈张雷, 章后甜, 刘新江. 临近空间高超声速飞行器天文导航系统综述[J]. 航空学报, 2020, 41(8): 623686-623686.
CHEN Bing, ZHENG Yong, CHEN Zhanglei, ZHANG Houtian, LIU Xinjiang. A review of celestial navigation system on near space hypersonic vehicle[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(8): 623686-623686.
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