Artículo
Spacecraft magnetic attitude control using approximating sequence Riccati equations
Autor/es | Rodríguez Vázquez, Antonio Leopoldo
Martín Prats, María de los Ángeles Bernelli Zazzera, Franco |
Departamento | Universidad de Sevilla. Departamento de Ingeniería Electrónica |
Fecha de publicación | 2015 |
Fecha de depósito | 2020-02-19 |
Publicado en |
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Resumen | This paper presents the results of a spacecraft attitude control system based on magnetic actuators designed for low Earth orbits. The control system is designed by using a nonlinear control technique based on the approximating ... This paper presents the results of a spacecraft attitude control system based on magnetic actuators designed for low Earth orbits. The control system is designed by using a nonlinear control technique based on the approximating sequence of Riccati equations. The behavior of the satellite is discussed under perturbations and model uncertainties. Simulation results are presented when the control system is able to guide the spacecraft to the desired attitude in a variety of different conditions. |
Cita | Rodríguez Vázquez, A.L., Martín Prats, M.d.l.Á. y Bernelli Zazzera, F. (2015). Spacecraft magnetic attitude control using approximating sequence Riccati equations. IEEE Transactions on Aerospace and Electronic Systems, 51 (4), 3374-3385. |
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