Abstract

This paper is concerned with the robust H2 tracking control problem for the yaw control of a small-scaled helicopter with time-varying uncertainty. The proposed controller incorporates an adaptation mechanism, which improves the performance of system compared with conventional robust controller with a fixed gain. Simulation results of the yaw control of a small-scaled helicopter mounted on an experiment platform have demonstrated the theoretic results.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.