Skip to Main Content
Skip Nav Destination
ASME Press Select Proceedings

International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3

Yi Xie
Yi Xie
Search for other works by this author on:
No. of Pages:
ASME Press
Publication date:

In this paper, we will consider designing the autopilot of an air to air missile using sliding mode control (SMC) based on fuzzy variable boundary layer. In sliding mode method, all system's states are guided toward a sliding surface through exerting a non-continuous control force on the dynamic system. This force and repeated switching produce chattering. To overcome this problem, Fuzzy control is applied to determine the boundary layer thickness. Therefore, the system is robust under various uncertainties and external disturbances.

This content is only available via PDF.
You do not currently have access to this chapter.
Close Modal

or Create an Account

Close Modal
Close Modal