前瞻科技 ›› 2022, Vol. 1 ›› Issue (1): 146-158.DOI: 10.3981/j.issn.2097-0781.2022.01.012
收稿日期:
2022-02-24
修回日期:
2022-03-03
出版日期:
2022-03-20
发布日期:
2022-04-21
作者简介:
王大轶,研究员,博士研究生导师。现任北京空间飞行器总体设计部科技委主任。国家杰出青年科学基金、国防科技卓越青年科学(首届)基金获得者,“973”项目技术首席专家,国务院政府特殊津贴专家,航天器自主运行技术学术带头人。长期从事自主导航和自主诊断重构技术的研究。获国家技术发明奖二等奖、国家科学技术进步奖特等奖、中国自动化学会自然科学奖一等奖、中国科协求是杰出青年奖、何梁何利基金科学与技术创新奖等。电子信箱: dayiwang@163.com。
基金资助:
WANG Dayi(), LI Jiaxing, DONG Tianshu, GE Dongming
Received:
2022-02-24
Revised:
2022-03-03
Online:
2022-03-20
Published:
2022-04-21
摘要:
深空探测任务具有探测目标远、飞行时间长、环境变化大等特点,传统的“地面测控站—航天器”大回路运行导航模式在实时性、安全性和可靠性等方面已无法满足任务需求,而自主导航技术是解决这些问题的有效手段,已成为未来深空探测发展的一个重要方向。为确保任务安全可靠,一般需要对关键的敏感器单机进行冗余容错设计,即采用多源融合的自主导航。文章分析了航天器多源融合自主导航关键技术的5个方面,包括相对动力学建模方法、可观测性理论、多源融合滤波方法、误差补偿方法和地面实验验证技术,结合自主导航工程实施和技术发展需求,提出未来航天器多源融合自主导航技术发展的趋势和重点。
王大轶, 李嘉兴, 董天舒, 葛东明. 基于航天器可观测性理论的多源融合自主导航技术[J]. 前瞻科技, 2022, 1(1): 146-158.
WANG Dayi, LI Jiaxing, DONG Tianshu, GE Dongming. Multi-source Fusion Autonomous Navigation Technologies Based on Spacecraft Observability Theory[J]. Science and Technology Foresight, 2022, 1(1): 146-158.
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