Cart (Loading....) | Create Account
Close category search window

Super-Maneuver Flight control design using constrained adaptive backstepping and sliding mode

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

5 Author(s)
Qin Shuo ; Aviation Theor. Dept., Air-force Aviation Univ., ChangChun, China ; Li You-Yi ; Yang Jun ; Xie Xin-Yue
more authors

Super-maneuver flight control is designed based on constrained backstepping and second-order sliding mode. A sort of MIMO second order sliding mode algorithm is designed. The main advantages of the Super-Maneuver flight control law combined backstepping and second order sliding mode are the prevention of chattering, higher accuracy and a significant simplification of the control law. The results of super-maneuver flight simulation show that the system achieves high dynamic and static performance and robustness.

Published in:

Control Conference (CCC), 2010 29th Chinese

Date of Conference:

29-31 July 2010

Need Help?

IEEE Advancing Technology for Humanity About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies

A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2014 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.