Abstract
In this paper, a Synergetic Control (SC) is proposed for a transformable quadrotor exposed to external disturbances. This control strategy has a simple structure, smooth dynamics and good tracking performance. The SC is applied to our system, which has the particularity of changing its morphology during the flight. Numerical simulations are performed to demonstrate the efficiency of the suggested control approach, of which a qualitative and quantitative comparison with respect to Sliding Mode Controller (SMC) is made. Overall, the investigations show that this control technique outperforms in terms of accuracy and robustness.
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 callSimilar Papers
More From: IFAC PapersOnLine
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.
