Abstract
The paper presents the dynamics of the servicing satellite. The model includes attitude and orbital dynamics of the satellite, with the goal to dock to the target satellite. The dynamics model is free of the singularities because of quaternion use. Orbital dynamics was defined in the internal reference frame with disturbances. To the satellite dynamic model the control system was proposed and the task was defined for the system was defined. Control algorithm was proposed based on Computed Torque control law. The new approach was to defined step by step procedure of the servicing mission of the telecommunication satellites.
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Jarzębowska, E., Szwajewski, M. (2017). Quaternion Based Dynamics for Servicing Satellite with Mission Protocol Description. In: Szewczyk, R., Kaliczyńska, M. (eds) Recent Advances in Systems, Control and Information Technology. SCIT 2016. Advances in Intelligent Systems and Computing, vol 543. Springer, Cham. https://doi.org/10.1007/978-3-319-48923-0_87
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DOI: https://doi.org/10.1007/978-3-319-48923-0_87
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