Abstract
This paper investigates a novel control strategy of addressing coupling issue for attitude tracking control of hypersonic flight vehicle. By using a defined coupling effect indicator which demonstrates whether a coupling harms or benefits the system, one finite-time coupling effect-triggered control scheme is proposed via applying the second-order sliding mode control technique. A specific nonlinear function is designed to implement the addition of beneficial couplings or removal of detrimental couplings. As a consequence, the proposed method establishes a unified couplings recognition and coupling effect-triggered control framework, which leads to a potential of improving the dynamic performance. The chattering attenuation is also involved for practical implementation. Finally, simulation results illustrate the validity of the proposed control scheme.
Sign-in/Register to access full text options 
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 callDisclaimer: 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.
