Affiliation:
1. Institute of Space Sciences, Shandong University, Weihai 264209, China
2. Qilu Aerospace Information Research Institute, Chinese Academy of Sciences, Jinan 250100, China
3. School of Systems Science and Engineering, Sun Yat-Sen University, Guangzhou 510275, China
Abstract
This study investigates and verifies the feasibility of the precise point positioning (PPP)-B2b enhanced real-time (RT) precise orbit determination (POD) of low Earth orbit (LEO) satellites. The principles and characteristics of matching various PPP-B2b corrections are introduced and analyzed. The performance and accuracy of broadcast ephemeris and PPP-B2b signals are compared and evaluated by referring to the precise ephemeris. The root mean square (RMS) errors in the Global Positioning System (GPS) and BeiDou Navigation Satellite System (BDS)-3 broadcast ephemeris orbits in the along direction are larger than those in the other two (radial and cross) directions, and correspondingly, the along component PPP-B2b corrections are greatest. The continuity and smoothness of the GPS and BDS-3 broadcast ephemeris orbits and clock offsets are improved with the PPP-B2b corrections. The availability of PPP-B2b corrections is comprehensively analyzed for the TJU-01 satellite. Several comparative schemes are adopted for the RT POD of the TJU-01 satellite using the broadcast ephemeris and PPP-B2b corrections. The RT POD performance is improved considerably with the broadcast ephemeris corrected by the PPP-B2b signals. The RMS of the RT orbital errors in the radial, along, and cross directions is 0.10, 0.13, and 0.09 m, respectively, using BDS-3 and GPS PPP-B2b corrections, with reference to the solutions calculated with the precise ephemeris. The accuracy is improved by 5.1%, 43.9%, and 28.7% in the three directions, respectively, relative to that achieved with the broadcast ephemeris. It is concluded that a greater proportion of received PPP-B2b satellite signals corresponds to a greater improvement in the accuracy of the RT POD of the LEO satellite.
Funder
National Natural Science Foundation of China
National Key Research and Development Program of China
Natural Science Foundation of Shandong Province
Reference28 articles.
1. Orbit determination system for the kompsat-2 using gps measurement data;Lee;Acta Astronaut.,2005
2. Precision real-time navigation of leo satellites using global positioning system measurements;Montenbruck;GPS Solut.,2007
3. Gps-based onboard real-time orbit determination for leo satellites using consider kalman filter;Yang;IEEE Trans. Aerosp. Electron. Syst.,2016
4. Reichert, A., Meehan, T., and Munson, T. (2002, January 4–7). Toward decimeter-level real-time orbit determination: A demonstration using the sac-c and champ spacecraft. Proceedings of the 15th International Technical Meeting of the Satellite Division of The Institute of Navigation (ION GPS 2002), Los Angeles, CA, USA.
5. (near-) real-time orbit determination for gnss radio occultation processing;Montenbruck;GPS Solut.,2013
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献