0410570 20240111140635.720060210235959.9 Nonlinear regulation for a helicopter model using error feedback London IEE 2000 CD-ROM UKACC International Conference on Control 2000 helicopter trajectory planning nonlinear output regulation cav_un_auth*0101183 Ramos-Velasco Luis Enrique UTIA-B Ústav teorie informace a automatizace AV ČR, v. v. i. cav_un_auth*0101074 Čelikovský Sergej UTIA-B Department of Control Theory Ústav teorie informace a automatizace AV ČR, v. v. i. cav_un_auth*0021094 Kučera V. CZ 198 kB 09I Beca CONACYT MX GA102/97/0861 GA ČR cav_un_auth*0004367 VS97034 GA MŠk cav_un_auth*0025111 AV0Z1075907 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. cav_un_auth*0212660 UKACC International Conference on CONTROL 2000 Cambridge GB 04.09.2000-07.09.2000 BC TŘ http://hdl.handle.net/11104/0130659 UTIA-B 20010039 2000 2000 London IEE 198 kB UKACC International Conference on Control 2000