Reconfigurable Nonlinear Dynamic Inversion for Attitude Control of a Structurally Damaged Aircraft

Reconfigurable Nonlinear Dynamic Inversion for Attitude Control of a Structurally Damaged Aircraft

Structural damage induces extensive parameter changes of an aircraft, which leads to the mismatch problem between the offline model and a flying aircraft. Due to extensive parameter changes, motion of a damaged aircraft is difficultly described with a mathematical model. This article uses disturbanc...

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Bibliographic Details
Main Authors: Qizhi He, Yi Tan, Xiaoxiong Liu, Qianlei Jia, Jinglong Liu
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Active fault-tolerant control
nonlinear dynamic inversion
nonlinear disturbance observer
reconfigurable controller
attitude control
adaptive control
Online Access:https://ieeexplore.ieee.org/document/9247109/

Internet

https://ieeexplore.ieee.org/document/9247109/

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