Integrated fault estimation and fault-tolerant control for a flexible regional aircraft
نویسندگان
چکیده
The article focuses on the design and application of an active reconfigurable controller that mitigates effects gust load actuator faults a flexible aircraft. A novel integrated adaptive output feedback scheme is investigated to address faults. real-time fault values provided by estimation module are considered in control law improve fault-tolerant capability. estimate gains calculated analyzing stability overall system. proposed simulated using aircraft model with discrete ‘1-cosine’ gust, results show it can effectively mitigate wing root moments recover flight maneuver after suffered from gusts.
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2022
ISSN: ['1000-9361', '2588-9230']
DOI: https://doi.org/10.1016/j.cja.2021.05.025