MATHEMATICAL DYNAMIC MODELING OF TWIN ROTOR MIMO AERODYNAMICAL SYSTEM
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216275%3A25530%2F10%3A39883361" target="_blank" >RIV/00216275:25530/10:39883361 - isvavai.cz</a>
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
MATHEMATICAL DYNAMIC MODELING OF TWIN ROTOR MIMO AERODYNAMICAL SYSTEM
Original language description
This paper presents the mathematical modelling of an experimental aerodynamical system, a twin-rotor multiple input-multiple output (MIMO) system (TRMAS). The system is modelled as two-degree-of-freedom (2DOF), respektive system is modelled one-degree-of-freedom (1DOF) in terms for vertical and horizontal parts. Modeling using Newtonian method. The modelling is separate in two phases. In the first phase described the d.c. motors, and his propulsive forces are modelled. Second part described vertical andhorizontal mechnical parts of the system.
Czech name
—
Czech description
—
Classification
Type
D - Article in proceedings
CEP classification
BC - Theory and management systems
OECD FORD branch
—
Result continuities
Project
—
Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Summaries volume 9th International Conference Process Control 2010
ISBN
978-80-7399-951-3
ISSN
—
e-ISSN
—
Number of pages
12
Pages from-to
—
Publisher name
Tribun EU
Place of publication
Brno
Event location
Kouty nad Desnou
Event date
Jun 7, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
—