Responses and suppression of Joined-Wing UAV in wind field based on distributed model and active disturbance rejection control-Reference-Cited by-同舟云学术

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Responses and suppression of Joined-Wing UAV in wind field based on distributed model and active disturbance rejection control

Published:2021-08 Issue: Volume:115 Page:106803
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Rui^ORCID,Zhou Zhou,Zhu Xiaoping,Wang Zhengping

Funder

Chinese Aeronautical Establishment Aeronautical Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. An overview of sensorcraft capabilities and key enabling technologies;Martinez,2008

2. The joined wing: an overview;Wolkovitch,1985

3. Joined wing sensorcraft aeroservoelastic wind tunnel test program;Reichenbach,2011

4. Active warping control of a Joined-Wing airplane configuration;Cesnik,2003

5. Application of active aeroelastic wing technology to a Joined-Wing sensorcraft;Reich;J. Aircr.,2004

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1. Flight test of flying wing aircraft controlled by dual synthetic jets at Ma0.2;Aerospace Science and Technology;2024-01

2. Flutter Characteristics of a Joined-Wing Unmanned Aerial Vehicle with Variable Dihedral Angles;AIAA Journal;2023-11

3. Least global position information based control of fixed-wing UAVs formation flight: Flight tests and experimental validation;Aerospace Science and Technology;2023-09

4. Modeling and analysis of a geometrically nonlinear joined wing under thrust force;Journal of Sound and Vibration;2023-02

5. Active disturbance rejection controller design for alleviation of gust-induced aeroelastic responses;Aerospace Science and Technology;2023-02

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