作业
发表于 2025-3-21 17:18:43
书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings影响因子(影响力)<br> http://impactfactor.cn/2024/if/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings影响因子(影响力)学科排名<br> http://impactfactor.cn/2024/ifr/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings网络公开度<br> http://impactfactor.cn/2024/at/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings网络公开度学科排名<br> http://impactfactor.cn/2024/atr/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings被引频次<br> http://impactfactor.cn/2024/tc/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings被引频次学科排名<br> http://impactfactor.cn/2024/tcr/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings年度引用<br> http://impactfactor.cn/2024/ii/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings年度引用学科排名<br> http://impactfactor.cn/2024/iir/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings读者反馈<br> http://impactfactor.cn/2024/5y/?ISSN=BK0225368<br><br> <br><br>书目名称China Satellite Navigation Conference (CSNC 2024) Proceedings读者反馈学科排名<br> http://impactfactor.cn/2024/5yr/?ISSN=BK0225368<br><br> <br><br>
为现场
发表于 2025-3-21 21:56:26
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云状
发表于 2025-3-22 02:52:17
Single Satellite Positioning Method and Error Characteristic Analysis of LEO Navigation Satellitesioning, this paper studies multi-epoch positioning method based on the idea of replacing time to space. Taking advantage of the characteristics of the LEO satellite, such as high angular velocity and high signal landing power, through limited time of navigation signal observation, the pseudo-range a
Instinctive
发表于 2025-3-22 07:45:43
A High Dynamic Positioning Algorithm for Ka Band LEO Satellites in Beam Polling Modellites in point beam polling mode, a LEO satellite/inertial integrated navigation and positioning algorithm based on accumulated error estimation and correction is proposed. A extended Kalman filtering estimator is used to achieve the state error estimation at the output of inertial navigation. By t
synovial-joint
发表于 2025-3-22 09:22:30
Spoofing Monitoring Method Research of GNSS Based on LEO Doppler Measurement support for constructing the future PNT system and improving its service performance. Spoofing is a potential factor to affect reliability of GNSS services, LEO satellites can provide reliable information as independent navigation sources and show good anti-spoofing performance with dual-direction
Recess
发表于 2025-3-22 13:36:58
Credibility Monitoring Research of BDS Based on LEO/INSare important factors affecting the reliability of airborne satellites navigation system. LEO satellites with advantages of running in low orbits, having rapid change of satellite geometry and strong anti-interference capability of satellite signal, can significantly enhance the credibility of BDS.
Recess
发表于 2025-3-22 17:42:37
ARAIM Integrity and Continuity Considering Fault Detection and Exclusiont satellites in view. However, there is a heightened likelihood of satellite fault occurrences, which can result in more mission interruptions and increase the continuity risk. In response, fault exclusion algorithms are indispensable to reducing the continuity risk and maintaining continuous naviga
帐单
发表于 2025-3-23 00:53:12
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有限
发表于 2025-3-23 03:10:34
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Catheter
发表于 2025-3-23 09:23:33
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