Abstract:In this paper, a fast power reaching law based sliding mode control with disturbance observer is presented to solve attitude tracking control problem for rigid spacecraft with the existence of inertia uncertainty and external disturbance. A disturbance observer is presented to estimate the lumped disturbance with bounded change rate. Then, a sliding mode controller is designed based on the fast power reaching law with considering disturbance estimation to ensure the convergence of the attitude and angular velo… Show more
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.