Design and Validation of Disturbance Rejection Dynamic Inverse Control for a Tailless Aircraft in Wind Tunnel

Design and Validation of Disturbance Rejection Dynamic Inverse Control for a Tailless Aircraft in Wind Tunnel

This paper focuses on the design of a disturbance rejection controller for a tailless aircraft based on the technique of nonlinear dynamic inversion (NDI). The tailless aircraft model mounted on a three degree-of-freedom (3-DOF) dynamic rig in the wind tunnel is modeled as a nonlinear affine system...

Full description

Bibliographic Details
Main Authors: Bowen Nie, Zhitao Liu, Tianhao Guo, Litao Fan, Hongxu Ma, Olivier Sename
Format: Article
Language:English
Published: MDPI AG 2021-02-01
Series:Applied Sciences
Subjects:
tailless aircraft
nonlinear dynamic inversion
disturbance observer
anti-windup
flight tests
wind tunnel
Online Access:https://www.mdpi.com/2076-3417/11/4/1407

Internet

https://www.mdpi.com/2076-3417/11/4/1407

Similar Items