Sequential Orbit Determination Verification for Geostationary Satellites

Date

2021-01-01

Author

KÖKER, ABDULKADİR
Tekinalp, Ozan
YILMAZ, ÜMİT CEZMİ
ŞAKACI, CEMAL

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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http://www.univelt.com/Advances.html
https://hdl.handle.net/11511/99881

Journal

Advances in Astronautical Sciences

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Department of Aerospace Engineering, Article

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SEQUENTIAL ORBIT DETERMINATION VERIFICATION FOR GEOSTATIONARY SATELLITES Köker, Abdulkadir; Tekinalp, Ozan; Yılmaz, Ü. Cezmi; Şakacı, Cemal (2021-01-01) © 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 compar...
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Citation Formats

A. KÖKER, O. Tekinalp, Ü. C. YILMAZ, and C. ŞAKACI, “Sequential Orbit Determination Verification for Geostationary Satellites,” Advances in Astronautical Sciences, vol. 175, pp. 3227–3244, 2021, Accessed: 00, 2022. [Online]. Available: http://www.univelt.com/Advances.html.