Basic performance and future developments of BeiDou global navigation satellite system

The core performance elements of global navigation satellite system include availability, continuity, integrity and accuracy, all of which are particularly important for the developing BeiDou global navigation satellite system (BDS-3). This paper describes the basic performance of BDS-3 and suggests some methods to improve the positioning, navigation and timing (PNT) service. The precision of the BDS-3 post-processing orbit can reach centimeter level, the average satellite clock offset uncertainty of 18 medium circular orbit satellites is 1.55 ns and the average signal-in-space ranging error is approximately 0.474 m. The future possible improvements for the BeiDou navigation system are also discussed. It is suggested to increase the orbital inclination of the inclined geostationary orbit (IGSO) satellites to improve the PNT service in the Arctic region. The IGSO satellite can perform part of the geostationary orbit (GEO) satellite’s functions to solve the southern occlusion problem of the GEO satellite service in the northern hemisphere (namely the “south wall effect”). The space-borne inertial navigation system could be used to realize continuous orbit determination during satellite maneuver. In addition, high-accuracy space-borne hydrogen clock or cesium clock can be used to maintain the time system in the autonomous navigation mode, and stability of spatial datum. Furthermore, the ionospheric delay correction model of BDS-3 for all signals should be unified to avoid user confusion and improve positioning accuracy. Finally, to overcome the vulnerability of satellite navigation system, the comprehensive and resilient PNT infrastructures are proposed for the future seamless PNT services.

[1]  Qile Zhao,et al.  Characteristics of BD3 Global Service Satellites: POD, Open Service Signal and Atomic Clock Performance , 2019, Remote. Sens..

[2]  Xin Li,et al.  Triple-frequency PPP Ambiguity Resolution with BDS-2 and BDS-3 Observations , 2018, Proceedings of the 31st International Technical Meeting of The Satellite Division of the Institute of Navigation (ION GNSS+ 2018).

[3]  Bin Wang,et al.  Performance of BDS-3: Measurement Quality Analysis, Precise Orbit and Clock Determination , 2017, Sensors.

[4]  Zhang Huijun,et al.  BDS-3 RNSS technical characteristics and service performance , 2019 .

[5]  Yuanxi Yang,et al.  Chinese geodetic coordinate system 2000 , 2009 .

[6]  Tianhe Xu,et al.  Comparing satellite orbit determination by batch processing and extended Kalman filtering using inter-satellite link measurements of the next-generation BeiDou satellites , 2019, GPS Solutions.

[7]  Paul Morantz,et al.  Dimensional characterization of a quasispherical resonator by microwave and coordinate measurement techniques , 2011 .

[8]  Zhang Qian Evaluation on the Precision of Klobuchar Model for BeiDou Navigation Satellite System , 2014 .

[9]  Yang Yuanxi,et al.  Performance Analysis of BDS Satellite Orbits during Eclipse Periods: Results of Satellite Laser Ranging Validation , 2016 .

[10]  Jingnan Liu,et al.  The contribution of intersatellite links to BDS ‐3 orbit determination: Model refinement and comparisons , 2019, Navigation.

[11]  J. Gabriel The Defense , 2013 .

[12]  Xiaoping Liu,et al.  Improved design of control segment in BDS‐3 , 2019, Navigation.

[13]  Zheng Yao,et al.  Overview of BDS III new signals , 2019, Navigation.

[14]  Zhiwu Cai,et al.  BeiDou Navigation Satellite System and its time scales , 2011 .

[15]  Yunbin Yuan,et al.  The BeiDou global broadcast ionospheric delay correction model (BDGIM) and its preliminary performance evaluation results , 2019, Navigation.

[16]  Xiaogong Hu,et al.  Comparison and analysis of two orbit determination methods for BDS-3 satellites , 2019 .

[17]  Bradford W. Parkinson,et al.  Global positioning system : theory and applications , 1996 .

[18]  Jinlong Li,et al.  Progress and performance evaluation of BeiDou global navigation satellite system: Data analysis based on BDS-3 demonstration system , 2018, Science China Earth Sciences.

[19]  O. Montenbruck,et al.  Chinese Navigation Satellite Systems , 2017 .

[20]  Haibo He,et al.  An analytical study on the carrier-phase linear combinations for triple-frequency GNSS , 2016, Journal of Geodesy.

[21]  Yuanxi Yang,et al.  Resilient PNT Concept Frame , 2020 .

[22]  Feng Zhang,et al.  Precise orbit determination for BDS-3 satellites using satellite-ground and inter-satellite link observations , 2019, GPS Solutions.

[23]  Yuan Yunbin,et al.  Performance Analysis of Different NeQuick Ionospheric Model Parameters , 2017 .

[24]  Yu-bin Wu,et al.  Concepts of Comprehensive PNT and Related Key Technologies , 2019, Proceedings of the 2019 International Conference on Modeling, Analysis, Simulation Technologies and Applications (MASTA 2019).

[25]  Yang Yuanxi Concepts of Comprehensive PNT and Related Key Technologies , 2016 .

[26]  Chengpan Tang,et al.  Inter-Satellite Link Enhanced Orbit Determination for BeiDou-3 , 2019, Journal of navigation.

[27]  Yue Mao,et al.  Introduction to BeiDou‐3 navigation satellite system , 2019, Navigation.

[28]  Yang Yuanxi,et al.  Micro-PNT and Comprehensive PNT , 2017 .

[29]  Tianhe Xu,et al.  Orbit determination of the Next-Generation Beidou satellites with Intersatellite link measurements and a priori orbit constraints , 2017 .