Application of CNS-INS integrated navigation technology in high-altitude aircraft

CHEN Hai-ming; XIONG Zhi; QIAO Li; HAN Ling

doi:10.13873/j.1000-97872008.09.005

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Application of CNS-INS integrated navigation technology in high-altitude aircraft

更新时间：2025-09-11

- Application of CNS-INS integrated navigation technology in high-altitude aircraft
- Issue 9, Pages: 4-6+10(2008)
- 作者机构：
  
  南京航空航天大学导航研究中心
- 作者简介：
- 基金信息：
- DOI：10.13873/j.1000-97872008.09.005
  CLC： V249.328
- Published：2008
- 稿件说明：
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[1]陈海明,熊智,乔黎,韩龄.天文—惯性组合导航技术在高空飞行器中的应用[J].传感器与微系统,2008(09):4-6+10.

CHEN Hai-ming, XIONG Zhi, QIAO Li, et al. Application of CNS-INS integrated navigation technology in high-altitude aircraft[J]. 2008, (9): 4-6+10.
[1]陈海明,熊智,乔黎,韩龄.天文—惯性组合导航技术在高空飞行器中的应用[J].传感器与微系统,2008(09):4-6+10. DOI： 10.13873/j.1000-97872008.09.005.

CHEN Hai-ming, XIONG Zhi, QIAO Li, et al. Application of CNS-INS integrated navigation technology in high-altitude aircraft[J]. 2008, (9): 4-6+10. DOI： 10.13873/j.1000-97872008.09.005.

摘要

综述了天文—惯性组合导航在高空飞行器中的应用和发展概况

在分析了国内外装载天文导航系统（CNS）/惯性导航系统（INS）的航空飞行器基础上

从工作环境、组合模式、导航解算等方面分析了CNS/INS的技术性能

指出CNSI-NS组合导航更适用于执行长航时、高空飞行的航空飞机

能够满足航空飞行器对高精度导航系统的需要。概括了CNS/INS导航的特有优点

提出了发展CNS-INS组合导航的必要性

讨论了今后机载CNS-INS组合导航技术的研究发展方向。

Abstract

The application and development of CNS-INS integrated navigation system in high-altitude aircrafrt are overviewed.On the basis of the analysis of aviation aircraft load celetid navigation system（CNS）/inertial navigation system（INS）integrated navigation system at home and abroad

the technical performance of CNS/INS integrated navigation system from working environment

integrated patterns and navigation solution is analyzed and it is pointed out that CNS-INS integrated navigation system is more applicable to the aviation aircraft of implementation of the long voyage and high-flying

it can meet the needs of aviation aircraft to high-precision navigation system.The unique advantages of CNS/INS integrated navigation system is summarized.The necessity of development of CNS-INS integrated navigation system is proposed

and the future research development direction for CNS-INS navigation technology on aircraft is discussed.

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references

SINS/CNS组合导航半实物仿真系统及其实验研究 [J]. 全伟,房建成. 系统仿真学报 . 2007(15)

天文导航技术的军事应用及发展 [J]. 于开峰,吴德伟,戚君宜. 国防技术基础 . 2006(07)

天文导航的发展历史、现状及前景 [J]. 陈义,程言. 中国水运(理论版) . 2006(06)

信息融合技术在组合导航系统中的应用 [J]. 李正强,王宏力,杨益强,刘春卓,陈琪. 飞行力学 . 2006(01)

高空长航时无人机SINS/CNS组合导航系统仿真研究 [J]. 吴海仙,俞文伯,房建成. 航空学报 . 2006(02)

国外天文导航技术发展综述 [J]. 何炬. 舰船科学技术 . 2005(05)

天文/惯性组合导航模式研究 [J]. 陈霞. 光学与光电技术 . 2003(03)

INS/CNS/GPS组合导航系统仿真研究 [J]. 李艳华,房建成,贾志凯. 中国惯性技术学报 . 2002(06)

天文导航与星光制导 [J]. 陈金枝. 舰船科学技术 . 2001(01)

高超声速巡航飞行器导航系统方案研究 [D]. 罗世杰. 西北工业大学 2006

航天器自主天文导航原理与方法[M]. 国防工业出版社 , 房建成,宁晓琳,田玉龙著, 2006

天文导航原理及应用[M]. 北京航空航天大学出版社 , 房建成等, 2006

Basic principles of celestial navigation [J] . James A. Van Allen. American Journal of Physics . 2004 (11)

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