Longitudinal directional flight control design using robust dynamic contraction method

Roman Czyba; Marian J. Blachuta

doi:10.1016/S1474-6670(17)35688-4

Longitudinal directional flight control design using robust dynamic contraction method

Department of Automatic Control and Robotics (RAU/RAU3)

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

Abstract

In the paper the design of an aircraft flight controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem of aerodynamic state variables: velocity of flight and flight path angle, which are responsible for aircraft flight conditions in the longitudinal movement. The applied DCM method allows to create the expected outputs for non-linear and non-stationary objects in spite of incomplete information about varying parameters of the system and external disturbances. The proposed technique is tested by simulations of a few maneuvers under wind gust for a F-16 aircraft model.

Original language	English
Pages (from-to)	347-352
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	36
Issue number	11
DOIs	https://doi.org/10.1016/S1474-6670(17)35688-4
Publication status	Published - 2003
Event	4th IFAC Symposium on Robust Control Design, ROCOND 2003 - Milan, Italy Duration: 25 Jun 2003 → 27 Jun 2003

Keywords

Aircraft control
Control system design
Disturbance signals
Nonlinear systems
Simulators

ASJC Scopus subject areas

Control and Systems Engineering

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10.1016/S1474-6670(17)35688-4

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title = "Longitudinal directional flight control design using robust dynamic contraction method",

abstract = "In the paper the design of an aircraft flight controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem of aerodynamic state variables: velocity of flight and flight path angle, which are responsible for aircraft flight conditions in the longitudinal movement. The applied DCM method allows to create the expected outputs for non-linear and non-stationary objects in spite of incomplete information about varying parameters of the system and external disturbances. The proposed technique is tested by simulations of a few maneuvers under wind gust for a F-16 aircraft model.",

keywords = "Aircraft control, Control system design, Disturbance signals, Nonlinear systems, Simulators",

author = "Roman Czyba and Blachuta, \{Marian J.\}",

note = "Publisher Copyright: {\textcopyright} 2003 IFAC.; 4th IFAC Symposium on Robust Control Design, ROCOND 2003 ; Conference date: 25-06-2003 Through 27-06-2003",

year = "2003",

doi = "10.1016/S1474-6670(17)35688-4",

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AU - Czyba, Roman

AU - Blachuta, Marian J.

PY - 2003

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N2 - In the paper the design of an aircraft flight controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem of aerodynamic state variables: velocity of flight and flight path angle, which are responsible for aircraft flight conditions in the longitudinal movement. The applied DCM method allows to create the expected outputs for non-linear and non-stationary objects in spite of incomplete information about varying parameters of the system and external disturbances. The proposed technique is tested by simulations of a few maneuvers under wind gust for a F-16 aircraft model.

AB - In the paper the design of an aircraft flight controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem of aerodynamic state variables: velocity of flight and flight path angle, which are responsible for aircraft flight conditions in the longitudinal movement. The applied DCM method allows to create the expected outputs for non-linear and non-stationary objects in spite of incomplete information about varying parameters of the system and external disturbances. The proposed technique is tested by simulations of a few maneuvers under wind gust for a F-16 aircraft model.

KW - Aircraft control

KW - Control system design

KW - Disturbance signals

KW - Nonlinear systems

KW - Simulators

UR - https://www.scopus.com/pages/publications/85064459543

U2 - 10.1016/S1474-6670(17)35688-4

DO - 10.1016/S1474-6670(17)35688-4

M3 - Conference article

AN - SCOPUS:85064459543

SN - 2405-8971

VL - 36

SP - 347

EP - 352

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

IS - 11

T2 - 4th IFAC Symposium on Robust Control Design, ROCOND 2003

Y2 - 25 June 2003 through 27 June 2003

ER -

Longitudinal directional flight control design using robust dynamic contraction method

Abstract

Keywords

ASJC Scopus subject areas

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