H∞ Tracking Control for Magnetically Controlled Nano-satellite

Neuro-fuzzy system based proportional derivative gain optimized attitude control of CubeSat under LEO perturbations

“…While to counter external disturbance, an H∞ controller scheme was proposed by Ref. [ 13 ] to create a state feedback attitude controller for magnetically actuated Nano-satellites. Hence, Fazlyab et al [ 14 ] developed a modified Rodrigues parameters feedback law based on a three-layered neural system for the estimation of obscure unsettling external disturbances and uncertainty in a dynamic model to handle the attitude control problem of the satellite.…”