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dc.contributor.authorBorque Gallego, Guzmán
dc.contributor.authorRossini, Leopoldo
dc.contributor.authorOnillon, Emmanuel
dc.contributor.authorKarimi, Alireza
dc.date.accessioned2022-02-14T17:07:47Z
dc.date.available2022-02-14T17:07:47Z
dc.date.issued2017
dc.identifier.citation2017 IEEE International Conference on Advanced Intelligent Mechatronics (AIM), Munich (Germany), pp. 1-5
dc.identifier.urihttps://yoda.csem.ch/handle/20.500.12839/670
dc.description.abstractThis paper presents a novel angular velocity estimation strategy of a Reaction Sphere (RS) for satellite attitude control based on a Linear Parameter-Varying (LPV) Kalman Filter. The reaction sphere is a permanent magnet synchronous spherical actuator whose rotor is magnetically levitated and can be accelerated about any desired axis. The spherical actuator is composed of an 8-pole permanent magnet spherical rotor and of a 20-coil stator. The proposed technique relies on the implementation of a Kalman Filter observer over a LPV state-space model based on the rotor dynamics and the spherical harmonic decomposition of the magnetic flux density generated by the rotor. First, a theoretical development of the aforementioned estimator will be exposed, followed by a description of simulation and experimental set-ups for the tests. Finally, the proposed estimator is compared with the previous method used for angular velocity estimation based on the estimation of the back-EMF voltages induced in the coils, obtaining a significant reduction in amplitude and frequency of oscillations in the angular velocity control loop.
dc.titleLinear Parameter-Varying Kalman Filter for angular velocity estimation of a reaction sphere actuator for satellite attitude control
dc.typeProceedings Article
dc.type.csemdivisionsDiv-E
dc.type.csemresearchareasScientific Instrumentation
dc.identifier.urlhttps://ieeexplore.ieee.org/document/8014042
dc.identifier.doi10.1109/AIM.2017.8014042


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