Abstract

In this paper, the fixed-time attitude tracking controller is proposed for rigid spacecraft subject to input deadzone and output constraint. Based on barrier Lyapunov function technique, a fixed-time controller is designed such that attitude tracking errors converge to zero within a fixed time while not exceeding the pre-specified boundaries in the presence of disturbance and input deadzone. The simulation reults are also provided to demonstrate the effectiveness of the designed fixed-time tracking control approach.

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.