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

Table 5

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

Performance index	Position	ATADRC	ABCADRC
MAE; (°/s)	Roll axis	0.00271354	0.00270116
	Pitch axis	0.00297974	0.00296033
	Yaw axis	0.00241845	0.00241320