Robust sliding-mode control for the uncertain MIMO aircraft model F-18

Elbrous M. Jafarov; Ramazan Tasaltin

doi:10.1109/7.892663

Robust sliding-mode control for the uncertain MIMO aircraft model F-18

Elbrous M. Jafarov, Ramazan Tasaltin

Department of Aeronautical Engineering

Istanbul Technical University

Research output: Contribution to journal › Article › peer-review

99 Citations (Scopus)

Abstract

Robust flight control laws based on variable structure control (VSC) theory and Lyapunov V-function method are designed for a simplified aircraft model F-18. A min-max control (MMC) and VSC laws are derived, for multi-input multi-output (MIMO) systems with plant uncertainties and input disturbance. Two types of robust feedback controllers MMC and VSC for uncertain MIMO systems are considered. For both cases the existence conditions of a stable sliding mode and the robust asymptotic stability in uncertain MIMO systems by MMC and VSC are investigated. For the design of an MMC and VSC, measurable states and sliding surface are chosen so that the zero dynamics of the system are stable. An application of tracking and positioning of VSC of longitudinal dynamics is presented. Finally, simulation results are presented to show the effectiveness of the design methods.

Original language	English
Pages (from-to)	1127-1141
Number of pages	15
Journal	IEEE Transactions on Aerospace and Electronic Systems
Volume	36
Issue number	4
DOIs	https://doi.org/10.1109/7.892663
Publication status	Published - Oct 2000

Access to Document

10.1109/7.892663

Cite this

@article{3c2909351216419390a14c307af3cbb6,

title = "Robust sliding-mode control for the uncertain MIMO aircraft model F-18",

abstract = "Robust flight control laws based on variable structure control (VSC) theory and Lyapunov V-function method are designed for a simplified aircraft model F-18. A min-max control (MMC) and VSC laws are derived, for multi-input multi-output (MIMO) systems with plant uncertainties and input disturbance. Two types of robust feedback controllers MMC and VSC for uncertain MIMO systems are considered. For both cases the existence conditions of a stable sliding mode and the robust asymptotic stability in uncertain MIMO systems by MMC and VSC are investigated. For the design of an MMC and VSC, measurable states and sliding surface are chosen so that the zero dynamics of the system are stable. An application of tracking and positioning of VSC of longitudinal dynamics is presented. Finally, simulation results are presented to show the effectiveness of the design methods.",

author = "Jafarov, {Elbrous M.} and Ramazan Tasaltin",

year = "2000",

month = oct,

doi = "10.1109/7.892663",

language = "English",

volume = "36",

pages = "1127--1141",

journal = "IEEE Transactions on Aerospace and Electronic Systems",

issn = "0018-9251",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

number = "4",

}

TY - JOUR

T1 - Robust sliding-mode control for the uncertain MIMO aircraft model F-18

AU - Jafarov, Elbrous M.

AU - Tasaltin, Ramazan

PY - 2000/10

Y1 - 2000/10

N2 - Robust flight control laws based on variable structure control (VSC) theory and Lyapunov V-function method are designed for a simplified aircraft model F-18. A min-max control (MMC) and VSC laws are derived, for multi-input multi-output (MIMO) systems with plant uncertainties and input disturbance. Two types of robust feedback controllers MMC and VSC for uncertain MIMO systems are considered. For both cases the existence conditions of a stable sliding mode and the robust asymptotic stability in uncertain MIMO systems by MMC and VSC are investigated. For the design of an MMC and VSC, measurable states and sliding surface are chosen so that the zero dynamics of the system are stable. An application of tracking and positioning of VSC of longitudinal dynamics is presented. Finally, simulation results are presented to show the effectiveness of the design methods.

AB - Robust flight control laws based on variable structure control (VSC) theory and Lyapunov V-function method are designed for a simplified aircraft model F-18. A min-max control (MMC) and VSC laws are derived, for multi-input multi-output (MIMO) systems with plant uncertainties and input disturbance. Two types of robust feedback controllers MMC and VSC for uncertain MIMO systems are considered. For both cases the existence conditions of a stable sliding mode and the robust asymptotic stability in uncertain MIMO systems by MMC and VSC are investigated. For the design of an MMC and VSC, measurable states and sliding surface are chosen so that the zero dynamics of the system are stable. An application of tracking and positioning of VSC of longitudinal dynamics is presented. Finally, simulation results are presented to show the effectiveness of the design methods.

UR - http://www.scopus.com/inward/record.url?scp=0034291385&partnerID=8YFLogxK

U2 - 10.1109/7.892663

DO - 10.1109/7.892663

M3 - Article

AN - SCOPUS:0034291385

SN - 0018-9251

VL - 36

SP - 1127

EP - 1141

JO - IEEE Transactions on Aerospace and Electronic Systems

JF - IEEE Transactions on Aerospace and Electronic Systems

IS - 4

ER -

Robust sliding-mode control for the uncertain MIMO aircraft model F-18

Abstract

Access to Document

Other files and links

Fingerprint

Cite this