Antisaturation fixed-time backstepping fuzzy integral sliding mode control for automatic landing of fixed-wing unmanned aerial vehicles-Reference-Cited by-同舟云学术

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Antisaturation fixed-time backstepping fuzzy integral sliding mode control for automatic landing of fixed-wing unmanned aerial vehicles

Published:2024-11 Issue:17 Volume:361 Page:107185
ISSN:0016-0032
Container-title:Journal of the Franklin Institute
language:en
Short-container-title:Journal of the Franklin Institute

Author:

Ebrahimpour MohammadReza^ORCID,Lungu Mihai^ORCID,Kakavand Marzieh

Publisher

Elsevier BV

Reference34 articles.

1. Modeling, autopilot design, and field tuning of a UAV with minimum control surfaces;Liu;IEEE Trans. Control Syst.,2015

2. Application Of H2/H∞ technique to aircraft landing control;Lungu;Asian J. Control,2015

3. Auto-landing of UAVs with variable centre of mass using the backstepping and dynamic inversion control;Lungu;Aerosp. Sci. Technol.,2020

4. Finite-time path following control for small-scale fixed-wing UAVs under wind disturbances;Yu;J. Frank. Inst.,2020

5. Robust cascaded horizontal-plane trajectory tracking for fixed-wing unmanned aerial vehicles;Yang;J. Frank. Inst.,2022

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