Abstract

The utilization of Global Navigation Satellite System (GNSS) is becoming an attractive navigation approach for geostationary orbit (GEO) satellites. A high-sensitivity receiver compatible with Global Position System (GPS) developed by the United States and BeiDou Navigation Satellite System (BDS) developed by China has been used in a GEO satellite named TJS-5 to demonstrate feasibility of real-time navigation. According to inflight data, the GNSS signal characteristics including availability, position dilution of precision (PDOP), carrier-to-noise ratio (C/N0), observations quantity and accuracy are analyzed. The mean number of GPS and GPS + BDS satellites tracked are 7.4 and 11.7 and the mean PDOP of GPS and GPS + BDS are 10.24 and 3.91, respectively. The use of BDS significantly increases the number of available navigation satellites and improves the PDOP. The number of observations with respect to C/N0 is illustrated in detail. The standard deviation of the pseudorange noises are less than 4 m, and the corresponding carrier phase noises are mostly less than 8 mm. We present the navigation performance using only GPS observations and GPS + BDS observations combination at different weights through comparisons with the precision reference orbits. When GPS combined with BDS observations, the root mean square (RMS) of the single-epoch least square position accuracy can improve from 32.1 m to 16.5 m and the corresponding velocity accuracy can improve from 0.238 m/s to 0.165 m/s. The RMS of real-time orbit determination position accuracy is 5.55 m and the corresponding velocity accuracy is 0.697 mm/s when using GPS and BDS combinations. Especially, the position accuracy in x-axis direction reduced from 7.24 m to 4.09 m when combined GPS with BDS observations.

Highlights

  • Nowadays, real-time orbit determination based on Global Navigation Satellite System (GNSS) is successfully used for geostationary orbit (GEO) satellites which traditionally depended on ground-based ranging systems

  • When Global Position System (GPS) combined with BeiDou Navigation Satellite System (BDS) observations, the root mean square (RMS) of the single-epoch least square position accuracy can improve from 32.1 m to 16.5 m and the corresponding velocity accuracy can improve from 0.238 m/s to 0.165 m/s

  • We investigate the flight signal characteristics in this GEO missions, considering GPS and BDS in terms of availability, position dilution of precision (PDOP), C/N0, the observation quantity and accuracy

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Summary

Introduction

Real-time orbit determination based on GNSS is successfully used for GEO satellites which traditionally depended on ground-based ranging systems. Because the power of side-lobe signals are generally about 20 dB lower than that of the main-lobe ones, we need to improve sensitivity of the receiver to process these signals [10,11,12] In spite of these difficulties, several feasibility studies for orbit determination with GNSS in GEO missions have been presented. Telecommunication Technology Test Satellite (TJS-5) was launched on 7 January 2020, and a high sensitivity GNSS receiver has been installed to realize tracking GPS and BDS signals and to perform orbit determination autonomously. We investigate the flight signal characteristics in this GEO missions, considering GPS and BDS in terms of availability, PDOP, C/N0, the observation quantity and accuracy. We give the performance evaluation of single-epoch least square solutions and real–time orbit determination solutions and discuss the contribution of BDS signals to GEO applications

Therefore
The filThe spaceborne receiver is shown in Figure
19 September 2012
Observations Quantity and Availability
19 Mayobservations
Availability
The nadir angles
Observations
17 May to on
Single-Point
4.92 GPS pseudorange
Results
Real-Time Orbit Determination Accuracy
Processing Model and Strategy
Analysis Results
Conclusions
Full Text
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