Robust nonlinear control of a hypersonic aircraft based on sliding mode control

Zhubing Hu; Bo Mo; Dezhi Zhou; Wenlong Han

doi:10.1016/j.proeng.2012.01.051

Robust nonlinear control of a hypersonic aircraft based on sliding mode control

Zhubing Hu^*, Bo Mo, Dezhi Zhou, Wenlong Han

^*Corresponding author for this work

School of Aerospace Engineering

Research output: Contribution to journal › Conference article › peer-review

5 Citations (Scopus)

Abstract

For the characteristic of the longitudinal model of a hypersonic aircraft containing strong coupling and uncertainty, a sliding mode controller with an improved approach exponential law, using feedback linear model was designed. The controller can solve the strong coupling and uncertainty of the longitudinal model, track the velocity step input and height step input with zero tracking error, and eliminate the control chattering. The control system has nice robustness.

Original language	English
Pages (from-to)	837-842
Number of pages	6
Journal	Procedia Engineering
Volume	29
DOIs	https://doi.org/10.1016/j.proeng.2012.01.051
Publication status	Published - 2012
Event	2012 International Workshop on Information and Electronics Engineering, IWIEE 2012 - Harbin, China Duration: 10 Mar 2012 → 11 Mar 2012

Keywords

Feedback linear
Hypersonic Aircraft
Robustness
Sliding mode control

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10.1016/j.proeng.2012.01.051

Cite this

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title = "Robust nonlinear control of a hypersonic aircraft based on sliding mode control",

abstract = "For the characteristic of the longitudinal model of a hypersonic aircraft containing strong coupling and uncertainty, a sliding mode controller with an improved approach exponential law, using feedback linear model was designed. The controller can solve the strong coupling and uncertainty of the longitudinal model, track the velocity step input and height step input with zero tracking error, and eliminate the control chattering. The control system has nice robustness.",

keywords = "Feedback linear, Hypersonic Aircraft, Robustness, Sliding mode control",

author = "Zhubing Hu and Bo Mo and Dezhi Zhou and Wenlong Han",

year = "2012",

doi = "10.1016/j.proeng.2012.01.051",

language = "English",

volume = "29",

pages = "837--842",

journal = "Procedia Engineering",

issn = "1877-7058",

publisher = "Elsevier B.V.",

note = "2012 International Workshop on Information and Electronics Engineering, IWIEE 2012 ; Conference date: 10-03-2012 Through 11-03-2012",

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T1 - Robust nonlinear control of a hypersonic aircraft based on sliding mode control

AU - Hu, Zhubing

AU - Mo, Bo

AU - Zhou, Dezhi

AU - Han, Wenlong

PY - 2012

Y1 - 2012

N2 - For the characteristic of the longitudinal model of a hypersonic aircraft containing strong coupling and uncertainty, a sliding mode controller with an improved approach exponential law, using feedback linear model was designed. The controller can solve the strong coupling and uncertainty of the longitudinal model, track the velocity step input and height step input with zero tracking error, and eliminate the control chattering. The control system has nice robustness.

AB - For the characteristic of the longitudinal model of a hypersonic aircraft containing strong coupling and uncertainty, a sliding mode controller with an improved approach exponential law, using feedback linear model was designed. The controller can solve the strong coupling and uncertainty of the longitudinal model, track the velocity step input and height step input with zero tracking error, and eliminate the control chattering. The control system has nice robustness.

KW - Feedback linear

KW - Hypersonic Aircraft

KW - Robustness

KW - Sliding mode control

UR - http://www.scopus.com/inward/record.url?scp=84858414043&partnerID=8YFLogxK

U2 - 10.1016/j.proeng.2012.01.051

DO - 10.1016/j.proeng.2012.01.051

M3 - Conference article

AN - SCOPUS:84858414043

SN - 1877-7058

VL - 29

SP - 837

EP - 842

JO - Procedia Engineering

JF - Procedia Engineering

T2 - 2012 International Workshop on Information and Electronics Engineering, IWIEE 2012

Y2 - 10 March 2012 through 11 March 2012

ER -

Robust nonlinear control of a hypersonic aircraft based on sliding mode control

Abstract

Keywords

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