A Low-speed, Low-acceleration Controller for Cost-effective Reaction-wheels

Design, Simulation & Implementation

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Abstract

With the requirements for CubeSats increasing, a push towards utilizing high­performance equipment has
never been greater. Incorporating these equipment in an environment that is cost­, space­ and
power­constrained, is challenging. Simultaneously, high­performance equipment require high
pointing­accuracy and low­jitter. This thesis proposes the use of a cost­effective reaction­wheel, which
utilizes three hall­sensors for accurate attitude­control. Additionally, the requirements state that the
reaction­wheel operates in the low­speed region, whilst tracking low­acceleration commands. For this, a
controller­structure is designed, simulated & implemented in order to provide accurate angular­velocity
estimates at a constant rate. Whilst the angular­velocity estimates are within 1% of the measurements, the
angular­acceleration tracking performance relies greatly on the noise of the reaction­wheel torque­friction.
Nonetheless, the angular­acceleration mean error was found to be 0.005 RPM/s, with a variance of 0.3
RPM/s on a 0.01 RPM/s reference

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MSc_Thesis_WALopes_4462653.pdf
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File under embargo until 22-12-2026