Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty

•This research emphasizes on an adaptive nonlinear integral-sliding-mode (ISM) controller design for F16 aircraft. The objective is to attain the desired maneuvering subject to the unknown external disturbance and aerodynamical uncertainty effects.•The nonlinear dynamics of F16 aircraft is first par...

Full description

Bibliographic Details

Published in:	Applied mathematics and computation Vol. 402; p. 126053
Main Authors:	Ijaz, Salman, Fuyang, Chen, Hamayun, Mirza Tariq, Anwaar, Haris
Format:	Journal Article
Language:	English
Published:	Elsevier Inc 01.08.2021
Subjects:	Adaptive control Nonlinear dynamic inversion Robustness Sliding mode control Uncertainty Uncertainty Robustness Nonlinear dynamic inversion Adaptive control Sliding mode control
ISSN:	0096-3003, 1873-5649
Online Access:	Get full text
Tags:	Add Tag No Tags, Be the first to tag this record!