Real-time Kinematic Orbit Determination of GRACE D Satellite Using GPS Broadcast Ephemeris
Author:
Affiliation:
1. Wuhan University,State Key Laboratory of Information Engineering in Surveying mapping and remote sense,Wuhan,China
Funder
National Natural Science Foundation of China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10318219/10318220/10318354.pdf?arnumber=10318354
Reference18 articles.
1. Real-Time Precise Orbit Determination for LEO between Kinematic and Reduced-Dynamic with Ambiguity Resolution
2. Swarm kinematic orbits and gravity fields from 18 months of GPS data;jäggi;Advances in Space Research,2015
3. Improved precise kinematic LEO orbits based on the raw observation approach
4. Enhancing the kinematic precise orbit determination of low earth orbiters using GPS receiver clock modelling
5. Real-Time Kinematic Precise Orbit Determination for LEO Satellites Using Zero-Differenced Ambiguity Resolution
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1. A Low Earth Orbit Satellite-Orbit Extrapolation Method Based on Multi-Satellite Ephemeris Coordination and Multi-Stream Fractional Autoregressive Integrated Moving Average;Aerospace;2024-09-11
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