Performance Assessment of a Turn Around Ranging in Communication Satellite Orbit Determination

Satellite operators utilize a two-stations turn around ranging (TAR) system to reduce the ground station measurement system's complexity and cost while having the same or better orbit determination accuracy for communication satellites orbit determination recently. This study investigates two stations' performance, four-way ranging on communication satellite orbit determination, operational conformance, and cost. The observation data sets are collected using traditional single station tracking (SST) and the new method TAR. The computed results using the Monte Carlo method encourage the satellite operators to use a four-way ranging system to observe and measure required data sets. TAR performance is evaluated, taking SST as a reference. The six classical orbital elements (a, e, i, RAAN, AoP, and TA) are compared for large numbers of observation data. The SST and TAR results are very close to each other. The worst-case calculated Euclidian distance between SST and TAR is 1.893 km at the epoch below the 6 km success criteria. The TAR observation method is appropriate to collect data sets for precise orbit determination. This work result indicates that satellite operators should consider deploying TAR stations to collect two-station range data sets and compute the orbit for nominal north-south station-keeping maneuvers (NSSK) and east-west station-keeping (EWSK) maneuver operations. The TAR method is superior to SST in terms of accuracy, operational conformance, and costs.

___

[1] M. Possner, F. F. Martinez , A. Agueda Mate, , G. Garcia, , C. N.Ping Choon, , W. Hasnibi, “Operational and performance aspects of a turn-around tracking system,” In SpaceOps 2010 Conference Delivering on the Dream Hosted by NASA Marshall Space Flight Center and Organized by AIAA, pp. 2374, 2010.

[2] O. Montenbruck, E. Gill, , F. Lutze, “Satellite orbits: models, methods, and applications,” Appl. Mech. Rev., 55(2), B27-B28, pp. 193-222, 2002.

[3] Soop, E. M.., “Angular tracking for geostationary orbits,” IFAC Proceedings, Volumes: 27, pp.181-186., 1994.

[4] I. Oz, , U. C. Yilmaz , “Determination of Coverage Oscillation for Inclined Communication Satellite,” Sakarya Üniversitesi Fen Bilimleri Enstitüsü Dergisi, 24(5), pp. 963-973, 2020.

[5] G. Bury, K. Sośnica, R. Zajdel, “Multi-GNSS orbit determination using satellite laser ranging,” Journal of Geodesy, 93(12), pp.2447-2463, 2019.

[6] Z. Qin, , G. Huang, Q.Zhang, L. Wang, X. Yan, , S. Xie, X. Wang, “Precise Orbit Determination for BeiDou GEO/IGSO Satellites during Orbit Maneuvering with Pseudo-Stochastic Pulses,” Remote Sensing, 11(21), 2587, 2019.

[7] Y. Gao, Z.You, , B. Xu, “Integrated Design of Autonomous Orbit Determination and Orbit Control for GEO Satellite Based on Neural Network,” International Journal of Aerospace Engineering, 2020.

[8] M. Li, J. Geng, C. Shi, Q. Zhao, “Orbit determination of geostationary satellite during maneuvers,” In International Conference on Earth Observation Data Processing and Analysis (ICEODPA), vol. 7285, pp. 728520, 2008.

[9] A. Águeda Maté, L. Strippoli, , J. Cuesta Cabanás, F. Martínez Fadrique, “SEGORD: Sequential Orbit Determination Tool for Geostationary Satellites Operations,”, In SpaceOps 2008 Conference, pp. 3206, 2008.

[10] M. Ibrahim, M. Zahara, A.Emam, M. A. Elghany, “Evaluation of Orbit Determination Using Dual Ranging Method,” In WSEAS International Conferences, 2007.

[11] I. Oz, “Evaluation of station location for orbit determination of geo satellites at different slots,” In 2017 8th International Conference on Recent Advances in Space Technologies (RAST), IEEE, pp. 375-379, 2017.

[12] H. D. Curtis, Orbital mechanics for engineering students. Butterworth-Heinemann., pp. 193- 254, 2013.

[13] M. Possner, F. Martinez Fadrique, A. Agueda Mate, G. Garcia, C. N. Ping Choon, W. Hasnibi, “Operational and performance aspects of a turn-around tracking system,” In SpaceOps 2010 Conference Delivering on the Dream Hosted by NASA Marshall Space Flight Center and Organized by AIAA, pp. 2374), 2010.

[14] C. Hajiyev, M. Ata, , “Error analysis of orbit determination for the geostationary satellite with single station antenna tracking data,” Positioning, vol:2(4), pp.135-144, 2011.

[15] Y. Hwang, B. S. Lee, H. Y. Kim, H. Kim, and J. Kim “Orbit determination accuracy improvement for geostationary satellite with single station antenna tracking data”, ETRI journal, 30(6), pp.774-782., 2008.

[16] M. Ibrahim, A. M. Abd El-Hameed, Z. Liang, H. Xingwei, “Analytical investigation for the satellite ranging data of changchun-SLR station”, NRIAG Journal of Astronomy and Geophysics, 9(1), 321-329, 2020.

[17] Y. Lv, T. Geng, Q. Zhao, X. Xie, F. Zhang, and X. Wang, “Evaluation of BDS-3 Orbit Determination Strategies Using Ground-Tracking and Inter-Satellite Link Observation”, Remote Sensing, 12(16), 2647, 2020.

[18] W. Wang, X. Yang, W. Li, Y. Ge, L. Chen, F. Cao, P. Wei, P. Liu and Z. Li, “Research on Evaluation Method of Time Transfer Performance Between Ground Stations in Two-Way Satellite Comparison Network”, IEEE Access, 9, 14038-14047, 2021.

[19] D. Vallado, “Orbit determination using ODTK version 6,” European Space Astronomy Centre (ESA/ESAC), Madrid, 2010.