Abstract
The paper proposes a coordinated adaptive control for the hypersonic reentry vehicle with channel coupling and system uncertainties. Using the hierarchical sliding mode scheme, the coordinated design is applied to ensure flight safety. Once the yawing moment is not enough to meet the control requirement, the system will coordinate the channel moment distribution, and furthermore, the flight attitude can be stabilized with yawing moment compensation. To obtain the high‐precision uncertain approximation, the online recorded data‐based prediction error is constructed as one learning performance index, which is introduced into the updated law. The uniformly ultimately boundedness of the system signals is guaranteed via the Lyapunov approach. Through the simulation test, the results show that the proposed approach can maintain a stable attitude and present the adaptation to the system uncertainty.
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.
