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.
In this paper, we investigate the tracking control of air-breathing hypersonic vehicles with a fast sliding mode controller. Based on the three order and four order subsystems after feedback linearization, new tracking error systems are developed. Subsequently, the nonsingular terminal sliding mode control is introduced to make that new error variables converge to zero in finite time. The time property...
Nonsingular terminal sliding mode control is widely accepted due to the properties of robust and finite time convergence. In this paper, the transient time of nonsingular terminal sliding mode is focused and deeply explored, where the transient time is exactly described by mathematic expressions. Simulation is executed on rigid manipulators to give the exact transient time when the system states converge...
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.