Neuro-fuzzy system based proportional derivative gain optimized attitude control of CubeSat under LEO perturbations
Heliyon
Heliyon ; 9 , 10 ; e20434
2023-10-01
Article (Journal)
Electronic Resource
English
Autonomous Neuro-Fuzzy Solution for Fault Detection and Attitude Control of a 3U Cubesat
BASE | 2015
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