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
media_type CD-ROM
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
source_size 198 kB
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
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