Abstract
An adaptive and sliding-mode observer (SMO) is designed for the incipient fault of guided missiles with unknown disturbance, which can not only estimate the incipient fault, but also have strong robustness against unknown disturbance. At first, the actuator fault and unknown disturbance are transformed into two subsystems by coordinate transformation; and then, an adaptive observer is designed to estimate the incipient fault for the subsystem which is free from disturbance, a sliding mode observer is designed to eliminate the effect of unknown disturbance for the subsystem which is affected by disturbance and incipient faults. At last, simulation results verify the efficiency of the proposed adaptive and sliding-mode observer based on incipient fault detection algorithm.
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.
