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

Table 3

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

Performance index	Position	ATADRC	ABCADRC
MAE; (°/s)	Roll axis	0.00265874	0.00264929
	Pitch axis	0.00291440	0.00289817
	Yaw axis	0.00237271	0.00237009
TT; (s)	Roll axis	441	440
	Pitch axis	473	470
	Yaw axis	420	417