The Infona portal uses cookies, i.e. strings of text saved by a browser on the user's device. The portal can access those files and use them to remember the user's data, such as their chosen settings (screen view, interface language, etc.), or their login data. By using the Infona portal the user accepts automatic saving and using this information for portal operation purposes. More information on the subject can be found in the Privacy Policy and Terms of Service. By closing this window the user confirms that they have read the information on cookie usage, and they accept the privacy policy and the way cookies are used by the portal. You can change the cookie settings in your browser.
Reliability analysis is important in the life cycle of safety critical Programmable Logic Controller (PLC) system. The complexity of PLC system reliability analysis arises in handling the complex relations between hardware components and embedded software. Different embedded software may lead to different arrangements of hardware execution and different system reliability quantities. In this paper,...
This paper is concerned with the design problem of robust fault-tolerant controller of linear uncertain satellite attitude control systems. The design method of output feedback robust fault-tolerant controller with failures of actuators and sensors is proposed to meet the given control performance by using LMI method. A numerical example of satellite attitude fault-tolerant control system is given...
In this paper, we study the global robust output regulation for a class of weakly minimum phase nonlinear systems. By employing the internal model design technique, we first convert the problem into a global robust stabilization problem of an augmented system whose structure has not been encountered before. Then we develop a methodology to solve this stabilization problem via state feedback, by utilizing...
This paper deals with attitude control of spacecraft with two moving-mass. Two mass particles are constrained to move in different circular track fixed within the spacecraft, respectively. The dynamical model of the spacecraft is presented in a reduced dimensional Hamiltonian form. The Hamiltonian model is noncanonical and underactuated. We consider the application of interconnection and damping assignment...
Set the date range to filter the displayed results. You can set a starting date, ending date or both. You can enter the dates manually or choose them from the calendar.