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dc.contributor.author | Murzabulatov, Alimzhan![]() |
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dc.date.accessioned | 2023-06-16T09:44:28Z | |
dc.date.available | 2023-06-16T09:44:28Z | |
dc.date.issued | 2023 | |
dc.identifier.citation | Murzabulatov, A. (2023). Design of an attitude control system for a CubeSat nanosatellite. School of Engineering and Digital Sciences | en_US |
dc.identifier.uri | http://nur.nu.edu.kz/handle/123456789/7229 | |
dc.description.abstract | The proposed research was carried out to design an appropriate non-linear controller for a non-linear time-variant model of a CubeSat nanosatellite. It is intended to experiment with a controller such as model predictive controller (MPC) to evaluate its performances and find out if it suits to the application. A complex simulation environment that includes spacecraft dynamics and environmental models was used to build the control law for the CubeSat's attitude control system. Tracking a group of state references that conform to a predetermined observation trajectory is the controller's goal. The controller was implemented in MATLAB simulation environment using ACADO toolkit | en_US |
dc.language.iso | en | en_US |
dc.publisher | School of Engineering and Digital Sciences | en_US |
dc.rights | Attribution-NonCommercial-ShareAlike 3.0 United States | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-sa/3.0/us/ | * |
dc.subject | Type of access: Restricted | en_US |
dc.subject | CubeSat nanosatellite | en_US |
dc.title | DESIGN OF AN ATTITUDE CONTROL SYSTEM FOR A CUBESAT NANOSATELLITE | en_US |
dc.type | Master's thesis | en_US |
workflow.import.source | science |
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