Abstract
This document describes the implementation of a state estimator, and an attitude controller for Advitiy, IIT Bombay’s 2nd Student Satellite. The algorithms used by the estimator and the controller are described. A closed-loop simulation (CLS) framework for the testing of these algorithms is explained. A detailed description of each of the blocks in CLS framework has been provided. The problems faced due to actuation with magnetorquer are described. It also contains the description of practices followed to ensure the quality (correctness of results obtained and repeatability of the process).
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Riya, Chirame, S., Joshi, A. A., Verma, R. M. K., Agrawal, S., Anand, R., … Parikh, N. (2020). Closed-Loop Simulation for Attitude Control of Nano-satellite. In Lecture Notes in Mechanical Engineering (pp. 87–97). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-15-1724-2_9
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