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

Table 6

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

Performance index	Position	ATADRC	ABCADRC
MAE; (°/s)	Roll axis	0.00272227	0.00271039
	Pitch axis	0.00298739	0.00296915
	Yaw axis	0.00242606	0.00242137