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

Table 2

Performance of robust fault-tolerant control for satellite attitude stabilization, respectively, based on ATADRC and ABCADRC under fault-free and environmental disturbance torques amplified by three times condition.

Performance index	Position	ATADRC	ABCADRC
MAE; (°/s)	Roll axis	0.00271791	0.00270576
	Pitch axis	0.00298355	0.00296472
	Yaw axis	0.00242225	0.00241728
TT; (s)	Roll axis	438	437
	Pitch axis	501	497
	Yaw axis	415	414