Neuro-variable structure flight control of reusable launch vehicles

D. H. XU; X. H. LIAO; Y. D. SONG

doi:10.1109/SSST.2005.1460919

Neuro-variable structure flight control of reusable launch vehicles

D. H. XU^*
, X. H. LIAO
, Y. D. SONG

^*Corresponding author for this work

Research output: Book Chapters | Papers in Conference Proceedings › Conference paper (refereed) › Research › peer-review

1 Citation (Scopus)

Abstract

This paper is concerned with the development of robust nonlinear control algorithms for Reusable Launch Vehicle (RLV), a highly nonlinear system with external disturbances and dynamic uncertainties due to varying flight conditions. A new robust control scheme for autopilot of RLV in both ascent and decent modes is derived. This scheme employs a rather simple algorithm and demands no linearization or estimation on any bounded function. Its effectiveness is verified via simulation. © 2005 IEEE.

Original language	English
Title of host publication	Proceedings of the Thirty-Seventh Southeastern Symposium on System Theory, SST05
Publisher	IEEE
Pages	267-271
Number of pages	5
ISBN (Print)	0780388089
DOIs	https://doi.org/10.1109/SSST.2005.1460919
Publication status	Published - 1 Dec 2005
Externally published	Yes
Event	The Thirty-Seventh Southeastern Symposium on System Theory, 2005. SSST '05. - Tuskegee University, Tuskegee, United States Duration: 20 Mar 2005 → 22 Mar 2005

Symposium

Symposium	The Thirty-Seventh Southeastern Symposium on System Theory, 2005. SSST '05.
Country/Territory	United States
City	Tuskegee
Period	20/03/05 → 22/03/05

Keywords

Neuro-variable Structure Control
Nonlinear Dynamics
Reusable Launch Vehicle
Trajectory Tracking

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10.1109/SSST.2005.1460919

Cite this

@inproceedings{2bad7c0690264f4799eb6ec0b8714a0b,

title = "Neuro-variable structure flight control of reusable launch vehicles",

abstract = "This paper is concerned with the development of robust nonlinear control algorithms for Reusable Launch Vehicle (RLV), a highly nonlinear system with external disturbances and dynamic uncertainties due to varying flight conditions. A new robust control scheme for autopilot of RLV in both ascent and decent modes is derived. This scheme employs a rather simple algorithm and demands no linearization or estimation on any bounded function. Its effectiveness is verified via simulation. {\textcopyright} 2005 IEEE.",

keywords = "Neuro-variable Structure Control, Nonlinear Dynamics, Reusable Launch Vehicle, Trajectory Tracking",

author = "XU, \{D. H.\} and LIAO, \{X. H.\} and SONG, \{Y. D.\}",

year = "2005",

month = dec,

day = "1",

doi = "10.1109/SSST.2005.1460919",

language = "English",

isbn = "0780388089",

pages = "267--271",

booktitle = "Proceedings of the Thirty-Seventh Southeastern Symposium on System Theory, SST05",

publisher = "IEEE",

note = "The Thirty-Seventh Southeastern Symposium on System Theory, 2005. SSST '05. ; Conference date: 20-03-2005 Through 22-03-2005",

}

XU, DH, LIAO, XH & SONG, YD 2005, Neuro-variable structure flight control of reusable launch vehicles. in Proceedings of the Thirty-Seventh Southeastern Symposium on System Theory, SST05., 1460919, IEEE, pp. 267-271, The Thirty-Seventh Southeastern Symposium on System Theory, 2005. SSST '05., Tuskegee, Alabama, United States, 20/03/05. https://doi.org/10.1109/SSST.2005.1460919

TY - GEN

T1 - Neuro-variable structure flight control of reusable launch vehicles

AU - XU, D. H.

AU - LIAO, X. H.

AU - SONG, Y. D.

PY - 2005/12/1

Y1 - 2005/12/1

N2 - This paper is concerned with the development of robust nonlinear control algorithms for Reusable Launch Vehicle (RLV), a highly nonlinear system with external disturbances and dynamic uncertainties due to varying flight conditions. A new robust control scheme for autopilot of RLV in both ascent and decent modes is derived. This scheme employs a rather simple algorithm and demands no linearization or estimation on any bounded function. Its effectiveness is verified via simulation. © 2005 IEEE.

AB - This paper is concerned with the development of robust nonlinear control algorithms for Reusable Launch Vehicle (RLV), a highly nonlinear system with external disturbances and dynamic uncertainties due to varying flight conditions. A new robust control scheme for autopilot of RLV in both ascent and decent modes is derived. This scheme employs a rather simple algorithm and demands no linearization or estimation on any bounded function. Its effectiveness is verified via simulation. © 2005 IEEE.

KW - Neuro-variable Structure Control

KW - Nonlinear Dynamics

KW - Reusable Launch Vehicle

KW - Trajectory Tracking

UR - https://www.scopus.com/pages/publications/33744918514

U2 - 10.1109/SSST.2005.1460919

DO - 10.1109/SSST.2005.1460919

M3 - Conference paper (refereed)

AN - SCOPUS:33744918514

SN - 0780388089

SP - 267

EP - 271

BT - Proceedings of the Thirty-Seventh Southeastern Symposium on System Theory, SST05

PB - IEEE

T2 - The Thirty-Seventh Southeastern Symposium on System Theory, 2005. SSST '05.

Y2 - 20 March 2005 through 22 March 2005

ER -

Neuro-variable structure flight control of reusable launch vehicles

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Keywords

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