Neuro-fuzzy system based proportional derivative gain optimized attitude control of CubeSat under LEO perturbations
Heliyon
Heliyon ; 9 , 10 ; e20434
01.10.2023
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Autonomous Neuro-Fuzzy Solution for Fault Detection and Attitude Control of a 3U Cubesat
BASE | 2015
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