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Influence of vibration in the airborne celestial navigation system on navigation accuracy
其他题名机载天文导航系统中振动对导航精度的影响
Dong, Qiang; Ma, Caiwen; Li, Yan; Yang, Xiaoxu; Yuan, Hui
2015-02-25
发表期刊Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University
卷号36期号:2页码:209-212
摘要For the issue of the influence of aircraft vibration on the navigation system positioning accuracy based on airborne autonomous celestial navigation system, an analysis of navigation platform vibration influenced from aircraft was preceded. Furthermore, a conclusion was given that the main factor is vibration angular displacement. Next, a single stellar positioning model in the celestial navigation system was established. According to the characteristics of vibration angular displacement, the similar coordinate transformation matrix in the angular displacement compensation was given. The results of vibration experiment and positioning model simulation validated that the angular vibration is the main error propagation to navigation system platform. The positioning error of celestial navigation system is 600 m when vibration angular displacement is 200 s along the x and y axis. ©, 2015, Editorial Board of Journal of HEU. All right reserved.
收录类别EI
语种中文
文献类型期刊论文
条目标识符http://ir.opt.ac.cn/handle/181661/27336
专题光电跟踪与测量技术研究室
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GB/T 7714
Dong, Qiang,Ma, Caiwen,Li, Yan,et al. Influence of vibration in the airborne celestial navigation system on navigation accuracy[J]. Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University,2015,36(2):209-212.
APA Dong, Qiang,Ma, Caiwen,Li, Yan,Yang, Xiaoxu,&Yuan, Hui.(2015).Influence of vibration in the airborne celestial navigation system on navigation accuracy.Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University,36(2),209-212.
MLA Dong, Qiang,et al."Influence of vibration in the airborne celestial navigation system on navigation accuracy".Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University 36.2(2015):209-212.
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