Abstract
Satellite navigation and monitoring, appearing as a component of the transport systems intellectualization, are based on spacecraft position control algorithms. The article presents a method for synthesis of optimal terminal control of angular velocities for an axisymmetric spacecraft based on the predicting model method. Analytical dependences for laws of control were also derived. The control actions and the spacecraft reactions were calculated using the derived analytical dependences. The control costs and terminal velocities values were also disclosed.
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Taran, V., Trofimenko, V. (2018). Transport Systems Intellectualization Based on Analytical Control Synthesis of Angular Velocities for the Axisymmetric Spacecraft. In: Abraham, A., Kovalev, S., Tarassov, V., Snasel, V., Vasileva, M., Sukhanov, A. (eds) Proceedings of the Second International Scientific Conference “Intelligent Information Technologies for Industry” (IITI’17). IITI 2017. Advances in Intelligent Systems and Computing, vol 680. Springer, Cham. https://doi.org/10.1007/978-3-319-68324-9_17
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DOI: https://doi.org/10.1007/978-3-319-68324-9_17
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