Research Article
A Modified Robust Adaptive Fault Compensation Design for Spacecraft with Guaranteed Transient Performance
Figure 3
Attitude tracking control using MMRAC-, SMRAC-, and DAC-based fault-tolerant control schemes for Case 2.
(a) Response of system output |
(b) Control input signals for different fault scenarios |
(c) Responses of tracking errors |
(d) System outputs for different in the MMAC design |