“…In [
24], actuator faults, external disturbances, and uncertain inertia parameter of a rigid spacecraft are regard as a lumped disturbance together, which is estimated via a finite‐time disturbance observer. Considering the coupling effect between the observer error dynamics and the control system, an
based adaptive observer is developed for nonlinear Lipschitz systems in the presence of external disturbances and actuator faults [
25]. More results on the fault diagnosis including the quantitative and qualitative methods for continuous‐time systems and discrete‐time systems can be found in [
26].…”