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...

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Vydané v:	Applied mathematics and computation Ročník 402; s. 126053
Hlavní autori:	Ijaz, Salman, Fuyang, Chen, Hamayun, Mirza Tariq, Anwaar, Haris
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Elsevier Inc 01.08.2021
Predmet:	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
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