Robust fixed-time flight controller for a dual-system convertible UAV in the cruise mode-Reference-Cited by-同舟云学术

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Robust fixed-time flight controller for a dual-system convertible UAV in the cruise mode

Published:2024-09 Issue: Volume:39 Page:53-66
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Chen Lulu^ORCID,Liu Zhenbao,Dang Qingqing,Zhao Wen,Chen Wenyu

Publisher

Elsevier BV

Reference42 articles.

1. A survey of hybrid unmanned aerial vehicles;Saeed;Prog Aero Sci,2018

2. Multidisciplinary design optimization of an electric propulsion system of a hybrid UAV considering wind disturbance rejection capability in the quadro- tor mode;Zhang;Aero Sci Technol,2021

3. Review of designs and flight control techniques of hybrid and convertible VTOL UAVs;Ducard;Aero Sci Technol,2021

4. Stability analysis for incremental nonlinear dy- namic inversion control;Wang;J Guid Control Dynam,2019

5. Auto-landing of fixed wing unmanned aerial vehicles using the backstepping control;Lungu;ISA Trans,2019

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