This study proposes a finite‐time integral backstepping control for a class of non‐linear systems considering practical aspects including saturation constraints, actuator fault …
This paper addresses the problem of attitude control of a spacecraft in the presence of model uncertainty, external disturbance, actuator fault and saturation. By introducing a novel …
In this article, an adaptive sliding mode control is used in the framework of fault tolerant control to mitigate the effects of actuator faults without requiring the actuator health …
SM Amrr, M Nabi - … of the Institute of Measurement and …, 2019 - journals.sagepub.com
This paper proposes a robust event-driven control for attitude regulation in flexible spacecraft affected by inertial parametric uncertainties and external disturbances. The …