Numerical simulation of satellite stabilization towards the Sun for the batteries charge is performed. The magnetic attitude control system implements the Sdot algorithm. It utilizes unprocessed Sun sensor measurements to compute the Sun direction vector derivative. Algorithm performance is discussed in view of onboard implementation specifics, eclipse occurrence, disturbances influence, and additional control measures.
Satellite Angular Motion under the Action of SDOT Magnetic One Axis Sun Acquisition Algorithm
Cosmic Res
Cosmic Research ; 59 , 6 ; 529-536
2021-11-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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