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Satellite Attitude Control Using Smart Approaching Index Switching Algorithm


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DOI: https://doi.org/10.15866/irease.v15i3.21893

Abstract


In this paper, a new Approaching Index Switching Algorithm (AISA) is used and implemented in attitude control in a micro-satellite testbed in order to improve the performance in terms of reducing errors, reducing the effort, and decreasing the settling time. AISA is designed to switch between two different control sets according to the value of the index. The first control represents the system output as fast as possible to reach the set value, and the other one represents the system output damping to reach the desired angle. A Reaction Wheel (RW) has been used to provide the required torque to rotate the satellite in one direction. The purpose of the controller is to change the speed of rotation of the RW to set the satellite in the appropriate direction. AISA has been applied and compared with Proportional-Derivative (PD) control in a practical model. Simulation and the testbed model of a closed-loop system show that all the desired specifications of the closed-loop (errors, stability, and power consumption) are robustly satisfied.
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Keywords


Modeling; Reaction Wheel; Attitude Control; Approaching Index Switching Algorithm

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References


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