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机载惯性/天文组合导航技术综述
引用本文:承德保,陆志东,岳亚洲. 机载惯性/天文组合导航技术综述[J]. 光学与光电技术, 2009, 7(3): 49-52
作者姓名:承德保  陆志东  岳亚洲
作者单位:北京航空航天大学经济管理学院,北京,100843;飞行自动控制研究所,陕西西安
摘    要:分析了惯性/天文组合导航的基本原理。针对航空机载应用平台,介绍了国内外天文导航设备和惯性/天文组合导航系统的研究现状,分析了我国在该领域的技术差距,探讨了未来机载惯性/天文组合导航技术的发展方向。

关 键 词:惯性/天文组合导航  惯性导航  天文导航

A Survey on Airborne Inertial-Celestial Integrated Navigation Technology
CHENG De-bao,LU Zhi-dong,YUE Ya-zhou. A Survey on Airborne Inertial-Celestial Integrated Navigation Technology[J]. optics&optoelectronic technology, 2009, 7(3): 49-52
Authors:CHENG De-bao  LU Zhi-dong  YUE Ya-zhou
Affiliation:1 Economy and Management School, Beihang University, Beijing 100843, China 2 Flight Automatic Control Research Institute, Xi'an 710065, China )
Abstract:The fundamental principles of the celestial navigation and the inertial-celestial integrated navigation are analysed in this paper. The development status of the celestial navigation equipments and the inertial-celestial integrated navigation system of airborne platforms at home and abroad are introduced. The future tendency of overseas airborne inertial-celestial integrated navigation technologies and our technology gap in this filed are discussed as well.
Keywords:celestial-inertial integrated navigation  inertial navigation  celestial navigation
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