Precise orbit determination of Beidou Satellites with precise positioning

Chuang Shi; Qile Zhao; Min Li; Weiming Tang; Zhigang Hu; Yidong Lou; Hongping Zhang; Xiaoji Niu; Jingnan Liu

doi:10.1007/s11430-012-4446-8

ScienceGate Book Chapters

JOURNAL ARTICLE

Precise orbit determination of Beidou Satellites with precise positioning

Chuang Shi Qile Zhao Min Li Weiming Tang Zhigang Hu Yidong Lou Hongping Zhang Xiaoji Niu Jingnan Liu

Year: 2012 Journal: Science China Earth Sciences Vol: 55 (7)Pages: 1079-1086 Publisher: Springer Science+Business Media

DOI: 10.1007/s11430-012-4446-8

Get Full-Text PDF Get Analytical Report

Keywords:

Precise Point Positioning BeiDou Navigation Satellite System Remote sensing Global Positioning System Computer science Orbit determination GNSS applications Real Time Kinematic Satellite Geodesy Dilution of precision Orbit (dynamics) Positioning system Quasi-Zenith Satellite System Differential GPS Satellite navigation Satellite system Point (geometry) Geology Telecommunications Physics Mathematics

Metrics

160

Cited By

40.70

FWCI (Field Weighted Citation Impact)

Refs

1.00

Citation Normalized Percentile

Is in top 1%

Is in top 10%

Citation History

Topics

GNSS positioning and interference

Physical Sciences → Engineering → Aerospace Engineering

Geophysics and Gravity Measurements

Physical Sciences → Earth and Planetary Sciences → Oceanography

Inertial Sensor and Navigation

Physical Sciences → Engineering → Aerospace Engineering

Precise orbit determination of Beidou Satellites with precise positioning

Metrics

Citation History

Topics

Related Documents

BeiDou Satellites Multi-GNSS Precise Orbit Determination with Ambiguity Fixed

Precise Orbit Determination for BeiDou Satellites During Eclipse Seasons

Precise Orbit Determination of BeiDou Satellites Using Satellite Laser Ranging

Performance Analysis of Beidou-2/Beidou-3e Combined Solution with Emphasis on Precise Orbit Determination and Precise Point Positioning

Precise Orbit Determination for BeiDou GEO/IGSO Satellites during Orbit Maneuvering with Pseudo-Stochastic Pulses