Robust Hover Mode Control of a Tiltrotor Using Nonlinear Control Technique

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F67985556%3A_____%2F16%3A00455662" target="_blank" >RIV/67985556:_____/16:00455662 - isvavai.cz</a>
Alternative codes found
RIV/68407700:21230/16:00237670
Result on the web
<a href="http://dx.doi.org/10.2514/6.2016-0359" target="_blank" >http://dx.doi.org/10.2514/6.2016-0359</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.2514/6.2016-0359" target="_blank" >10.2514/6.2016-0359</a>

Result language
angličtina
Original language name
Robust Hover Mode Control of a Tiltrotor Using Nonlinear Control Technique
Original language description
Tiltrotor aircraft are complex, highly nonlinear systems which offers distinct operational advantages due to their unique Vertical Take-Off and Landing (VTOL) capabilities. Hovering a piloted tiltrotor in the helicopter flight condition is one of the most challenging tasks for pilots. Therefore, automatic control of the tiltrotor is always desired. Classical automatic linear control techniques fail to provide an adequate performance guarantee. In comparison, the application of nonlinear control techniques offers a potential alternative. Thus, in this paper modelling and hover control of a BELL XV-15 tiltrotor aircraft is presented. The MATLAB/Simulink based dynamic model of the BELL XV-15 tiltrotor aircraft is validated with respect to FLIGHTLAB model.In addition, a nonlinear hierarchical control strategy is adopted to provide automatic hover control of the tiltrotor aircraft. The results show a good hovering performance of the tiltrotor aircraft with small position tracking error.
Czech name
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Czech description
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Project
<a href="/en/project/GA13-20433S" target="_blank" >GA13-20433S: Analysis and control of globally decomposed strongly nonlinear state space dynamical models with complex interactions of their components</a><br>
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
AIAA Guidance, Navigation, and Control Conference
ISBN
978-1-62410-389-6
ISSN
—
e-ISSN
—
Number of pages
16
Pages from-to
1-16
Publisher name
AIAA SciTech
Place of publication
San Diego
Event location
San Diego, California
Event date
Jan 4, 2016
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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