Multidisciplinary design optimization of an electric propulsion system of a hybrid UAV considering wind disturbance rejection capability in the quadrotor mode-Reference-Cited by-同舟云学术

Multidisciplinary design optimization of an electric propulsion system of a hybrid UAV considering wind disturbance rejection capability in the quadrotor mode

Published:2021-03 Issue: Volume:110 Page:106372
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Hang,Song Bifeng,Li Fan,Xuan Jianlin

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

China Postdoctoral Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

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2. Attitude and altitude stabilization of fixed wing VTOL unmanned air vehicle;Anil,2016

3. Design and fabrication of small vertical-take-off-landing unmanned aerial vehicle;Abd Rahman;MATEC Web Conf.,2018

4. Development of a quad-rotor fixed-wing hybrid unmanned aerial vehicle;Gunarathna,2018

5. Retrospective cost adaptive PID control of quadcopter/fixed-wing mode transition in a VTOL aircraft;Ahmad,2018

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