ATTITUDE CONTROL AND STABILIZATION OF SATELLITES USING REACTION WHEELS
DOI:
https://doi.org/10.62985/j.huit_ojs.vol26.no2E.393Keywords:
Satellite, attitude control, stabilization, reaction wheel, MATLAB/Simulink, Monte Carlo simulationAbstract
This paper presents a study on the dynamic modeling of a satellite–reaction wheel system in MATLAB/Simulink, the design and optimization of the controller using Simulink Design Optimization, and the assessment of system accuracy and stability under random disturbance torques via Monte Carlo simulations. The results provide a basis for further research on satellite attitude control and stabilization systems.
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