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Attitude Determination and Control System Open-Source Simulator of a 1U CubeSat Nanosatellite
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Orientador(es)
Resumo(s)
This work developed an open-source educational simulator to evaluate control schemes for small CubeSat-class satellites of 1U size (1 unit). Attitude (orientation) estimation was achieved using the Three-Axis Attitude Determination (TRIAD) algorithm, commonly employed in competitions and real-world CubeSats. A simple Proportional (P) controller was designed to regulate the CubeSat's angular velocity. Additionally, for pointing control (line-of-sight orientation), a Proportional-Derivative (PD) controller was implemented. Numerical simulations were conducted to assess the performance of the CubeSat's Attitude Determination and Control Subsystem (ADCS).
Descrição
Palavras-chave
CubeSat TRIAD Algorithm Modified PD controller Attitude determination Open-Source software
Contexto Educativo
Citação
Resende, Túlio Santos; Silva, Josué Lima da; Peixoto, Alessandro Jacoud; Santos, Murillo Ferreira dos; Pereira, Ana I.; Lima, José; Morais, Maurício Herche Fófano de (2025). Attitude Determination and Control System Open-Source Simulator of a 1U CubeSat Nanosatellite. In 26th International Carpathian Control Conference, ICCC 2025. Stary Smokovec:IEEE. p. 1-6. ISBN 979-833150127-3
Editora
Institute of Electrical and Electronics Engineers