Zengshan Yin
Abstract
Based on simulation of on board GPS receiver data,five datasets of GPS receiver are produced at different sampling rates.With basic dynamical models and measurement models,precision orbit determination(POD)of GPS simulation datasets is carried out.Errors for spacecraft POD are presented for circumstances of different GPS sampling rates.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Based on simulation of on board GPS receiver data,five datasets of GPS receiver are produced at different sampling rates.With basic dynamical models and measurement models,precision orbit determination(POD)of GPS simulation datasets is carried out.Errors for spacecraft POD are presented for circumstances of different GPS sampling rates.
Key concepts: Global Positioning System, Orbit determination, Spacecraft, Gps receiver, Sampling (signal processing), Precision Lightweight GPS Receiver, Geodesy, Remote sensing