Robust Fault-Tolerant Control for Satellite Attitude Stabilization Based on Active Disturbance Rejection Approach with Artificial Bee Colony Algorithm

Table 4

Performance of robust fault-tolerant control for satellite attitude stabilization, respectively, based on ATADRC and ABCADRC under measurement uncertainty condition.

Performance index	Position	ATADRC	ABCADRC
MAE; (°/s)	Roll axis	0.00271919	0.00270355
	Pitch axis	0.00298260	0.00296581
	Yaw axis	0.00241643	0.00241018
TT; (s)	Roll axis	438	436
	Pitch axis	499	499
	Yaw axis	413	413