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SEQUENTIAL ORBIT DETERMINATION VERIFICATION FOR GEOSTATIONARY SATELLITES
Date
2021-01-01
Author
Köker, Abdulkadir
Tekinalp, Ozan
Yılmaz, Ü. Cezmi
Şakacı, Cemal
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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© 2021, Univelt Inc. All rights reserved.Sequential orbit determination using angle and range measurements for geostationary satellites is presented. The approach includes position, velocity and bias estimation with Unscented Kalman Filter. The measurements are taken from the actual ground station antennas at TURKSAT. In order to evaluate the accuracy and the robustness of the system, estimation is repeated with single and multiple ground station measurements for satellite T4B. Estimation results are compared with the reference orbit determination software and a very good agreement is obtained.
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85126197247&origin=inward
https://hdl.handle.net/11511/99220
Conference Name
AAS/AIAA Astrodynamics Specialist Conference, 2020
Collections
Department of Aerospace Engineering, Conference / Seminar
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A. Köker, O. Tekinalp, Ü. C. Yılmaz, and C. Şakacı, “SEQUENTIAL ORBIT DETERMINATION VERIFICATION FOR GEOSTATIONARY SATELLITES,” Virtual, Online, 2021, vol. 175, Accessed: 00, 2022. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85126197247&origin=inward.
