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The aim of this thesis will be modelling of the Rosetta spacecraft, including its relevant parts within Consert Unit and Philae Lander. For realize this subject, Feko code has been used, which is based on Method of Moments to determine radiation coupling effects and secondary propagation paths.
Raquel Luna Macia
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Accuracy Analysis of the Calibration Satellite Orbit Determination Based on Onboard BDS Data
Lecture Notes in Electrical Engineering, 2021Yanan Fang
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Natural Intermediaries as Onboard Orbit Propagators
2nd IAA Conference on Dynamics and Control of Space Systems, 2014Gurfil, P, Lara, M
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Localized Density/Drag Prediction for Improved Onboard Orbit Propagation
Nathan Stastny +5 more
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GPS and SGP4 based Orbit Propagation onboard the Galassia-2 Nanosatellite
Luo Sha +4 more
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GPS-based onboard real-time orbit determination for leo satellites using consider Kalman filter
IEEE Transactions on Aerospace and Electronic Systems, 2016Yang Yang +2 more
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