| bibtype |
C -
Conference Paper (international conference)
|
| ARLID |
0410395 |
| utime |
20240111140635.6 |
| mtime |
20060210235959.9 |
| title
(primary) (eng) |
Robust regulation via sliding modes of a helicopter model |
| publisher |
| place |
Praha |
| name |
ÚTIA AV ČR |
| pub_time |
2000 |
|
| specification |
|
| serial |
| title
|
Preprints of the 3rd IFAC Symposium on Robust Control Design |
|
| author
(primary) |
| ARLID |
cav_un_auth*0101183 |
| name1 |
Ramos-Velasco |
| name2 |
Luis Enrique |
| institution |
UTIA-B |
| fullinstit |
Ústav teorie informace a automatizace AV ČR, v. v. i. |
|
| author
|
| ARLID |
cav_un_auth*0101074 |
| name1 |
Čelikovský |
| name2 |
Sergej |
| institution |
UTIA-B |
| full_dept |
Department of Control Theory |
| fullinstit |
Ústav teorie informace a automatizace AV ČR, v. v. i. |
|
| author
|
| ARLID |
cav_un_auth*0021094 |
| name1 |
Kučera |
| name2 |
V. |
| country |
CZ |
|
| source |
|
| COSATI |
09I |
| cas_special |
| project |
| project_id |
GA102/97/0861 |
| agency |
GA ČR |
| ARLID |
cav_un_auth*0004367 |
|
| research |
AV0Z1075907 |
| abstract
(eng) |
The laboratory model of the helicopter with two degrees of freedom is studied here. Based on its model, the problem of output regulation is considered. Sliding modes technique enables to obtain robust results. Simulations confirm expected results. |
| action |
| ARLID |
cav_un_auth*0212678 |
| name |
ROCOND 2000 /3./ |
| place |
Praha |
| country |
CZ |
| dates |
21.06.2000-23.06.2000 |
|
| RIV |
BC |
| department |
TŘ |
| permalink |
http://hdl.handle.net/11104/0130484 |
| ID_orig |
UTIA-B 20000111 |
| arlyear |
2000 |
| mrcbU10 |
2000 |
| mrcbU10 |
Praha ÚTIA AV ČR |
| mrcbU56 |
212 kB |
| mrcbU63 |
Preprints of the 3rd IFAC Symposium on Robust Control Design |
|