Sliding mode control for a dynamic system, helicopter type

Bogdan Codres; Gheorghe Puscasu; Gabriel Murariu; Alexandru Codres; Alexandru Stancu

doi:10.1109/ISEEE.2013.6674322

Sliding mode control for a dynamic system, helicopter type

Bogdan Codres, Gheorghe Puscasu, Gabriel Murariu, Alexandru Codres, Alexandru Stancu

Research output: Chapter in Book/Conference proceeding › Conference contribution

Abstract

This paper presents a sliding mode control structure designed for a dynamic system, helicopter type. The approach is robust to model uncertainties and disturbances. The proposed control algorithm is validated on a laboratory stand which uses carrying force to stabilize a helicopter. © 2013 IEEE.

Original language	English
Title of host publication	2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 - Proceedings\|Int. Symp. Electr. Electron. Eng., ISEEE - Proc.
Publisher	IEEE Computer Society
DOIs	https://doi.org/10.1109/ISEEE.2013.6674322
Publication status	Published - 2013
Event	2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 - Galati Duration: 1 Jul 2013 → … http://www.scopus.com/inward/record.url?eid=2-s2.0-84899015675&partnerID=40&md5=87f3e611ad8043a48766f900399cdc65

Conference

Conference	2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013
City	Galati
Period	1/07/13 → …
Internet address	http://www.scopus.com/inward/record.url?eid=2-s2.0-84899015675&partnerID=40&md5=87f3e611ad8043a48766f900399cdc65

Keywords

control
identification
sliding mode

Access to Document

10.1109/ISEEE.2013.6674322

Cite this

@inproceedings{81348c0d10df4a2fb5bd6b0d5f369a88,

title = "Sliding mode control for a dynamic system, helicopter type",

abstract = "This paper presents a sliding mode control structure designed for a dynamic system, helicopter type. The approach is robust to model uncertainties and disturbances. The proposed control algorithm is validated on a laboratory stand which uses carrying force to stabilize a helicopter. {\textcopyright} 2013 IEEE.",

keywords = "control, identification, sliding mode",

author = "Bogdan Codres and Gheorghe Puscasu and Gabriel Murariu and Alexandru Codres and Alexandru Stancu",

note = "cited By (since 1996)0; 2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 ; Conference date: 01-07-2013",

year = "2013",

doi = "10.1109/ISEEE.2013.6674322",

language = "English",

booktitle = "2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 - Proceedings|Int. Symp. Electr. Electron. Eng., ISEEE - Proc.",

publisher = "IEEE Computer Society ",

address = "United States",

url = "http://www.scopus.com/inward/record.url?eid=2-s2.0-84899015675&partnerID=40&md5=87f3e611ad8043a48766f900399cdc65",

}

Codres, B, Puscasu, G, Murariu, G, Codres, A & Stancu, A 2013, Sliding mode control for a dynamic system, helicopter type. in 2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 - Proceedings|Int. Symp. Electr. Electron. Eng., ISEEE - Proc.. IEEE Computer Society , 2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013, Galati, 1/07/13. https://doi.org/10.1109/ISEEE.2013.6674322

Sliding mode control for a dynamic system, helicopter type. / Codres, Bogdan; Puscasu, Gheorghe; Murariu, Gabriel et al.
2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 - Proceedings|Int. Symp. Electr. Electron. Eng., ISEEE - Proc.. IEEE Computer Society , 2013.

Research output: Chapter in Book/Conference proceeding › Conference contribution

TY - GEN

T1 - Sliding mode control for a dynamic system, helicopter type

AU - Codres, Bogdan

AU - Puscasu, Gheorghe

AU - Murariu, Gabriel

AU - Codres, Alexandru

AU - Stancu, Alexandru

N1 - cited By (since 1996)0

PY - 2013

Y1 - 2013

N2 - This paper presents a sliding mode control structure designed for a dynamic system, helicopter type. The approach is robust to model uncertainties and disturbances. The proposed control algorithm is validated on a laboratory stand which uses carrying force to stabilize a helicopter. © 2013 IEEE.

AB - This paper presents a sliding mode control structure designed for a dynamic system, helicopter type. The approach is robust to model uncertainties and disturbances. The proposed control algorithm is validated on a laboratory stand which uses carrying force to stabilize a helicopter. © 2013 IEEE.

KW - control

KW - identification

KW - sliding mode

U2 - 10.1109/ISEEE.2013.6674322

DO - 10.1109/ISEEE.2013.6674322

M3 - Conference contribution

BT - 2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013 - Proceedings|Int. Symp. Electr. Electron. Eng., ISEEE - Proc.

PB - IEEE Computer Society

T2 - 2013 4th International Symposium on Electrical and Electronics Engineering, ISEEE 2013

Y2 - 1 July 2013

ER -

Sliding mode control for a dynamic system, helicopter type

Abstract

Conference

Keywords

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