Abstract
In order to obtain the optical tradition of the satellite path, traditional orbital elements must be obtained. In recent years, models and simulation of spacecraft have been developed. The aim of this research paper is to demonstrate the detailed reliability and adequacy of simulations, which can be obtained using cable or neutral factors rather than the Cartesian’ coordinates accordingly to the state-consistent pattern of the spacecraft. The solid body pattern of the Multibody’s standard library is expanded by adding equations that determine the centre of the body’s transformation of cluster coordinates from Keplerian variables to Cartesian coordinates, and by assigning identified cases. The remaining parts of the model, including the gravitational field pattern, are left intact, ensuring a severe reuse of the system. The results shown in the paper show the super-precision and the calculation of the six elements in the case of reference to the gravitational field of the cluster point and the strong visualization of satellite tracking.
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This research was supported by a TEDDSAT Project grant, Egypt.
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Ezzat, K.A., Mahdy, L.N., Hassanien, A.E., Darwish, A. (2019). Robust Simulation and Visualization of Satellite Orbit Tracking System. In: Hassanien, A., Tolba, M., Shaalan, K., Azar, A. (eds) Proceedings of the International Conference on Advanced Intelligent Systems and Informatics 2018. AISI 2018. Advances in Intelligent Systems and Computing, vol 845. Springer, Cham. https://doi.org/10.1007/978-3-319-99010-1_46
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