Research Article

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

Figure 15

Simulation result of attitude stabilization with ATADRC under flywheel fault and environmental disturbance torque amplified by five times condition.
512707.fig.0015a
(a) Attitude angles
512707.fig.0015b
(b) Control torque supplied by the four flywheels