bibtype |
C -
Conference Paper (international conference)
|
ARLID |
0410570 |
utime |
20240111140635.7 |
mtime |
20060210235959.9 |
title
(primary) (eng) |
Nonlinear regulation for a helicopter model using error feedback |
publisher |
place |
London |
name |
IEE |
pub_time |
2000 |
|
specification |
|
serial |
title
|
UKACC International Conference on Control 2000 |
|
keyword |
helicopter |
keyword |
trajectory planning |
keyword |
nonlinear output regulation |
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 |
Beca |
agency |
CONACYT |
country |
MX |
|
project |
project_id |
GA102/97/0861 |
agency |
GA ČR |
ARLID |
cav_un_auth*0004367 |
|
project |
project_id |
VS97034 |
agency |
GA MŠk |
ARLID |
cav_un_auth*0025111 |
|
research |
AV0Z1075907 |
abstract
(eng) |
A problem of output regulation of the laboratory model of the helicopter is considered here. The model has two degrees of freedom and was provided by HUMOSOFT Ltd. Nonlinear output regulation theory is applied here and the performance of a proposed feedback regulator is tested using digital computer simulations. |
action |
ARLID |
cav_un_auth*0212660 |
name |
UKACC International Conference on CONTROL 2000 |
place |
Cambridge |
country |
GB |
dates |
04.09.2000-07.09.2000 |
|
RIV |
BC |
department |
TŘ |
permalink |
http://hdl.handle.net/11104/0130659 |
ID_orig |
UTIA-B 20010039 |
arlyear |
2000 |
mrcbU10 |
2000 |
mrcbU10 |
London IEE |
mrcbU56 |
198 kB |
mrcbU63 |
UKACC International Conference on Control 2000 |
|