Controller design for highly maneuverable aircraft technology using structured singular value and direct search method
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F20%3A63526129" target="_blank" >RIV/70883521:28140/20:63526129 - isvavai.cz</a>
Result on the web
<a href="https://ieeexplore.ieee.org/document/9214017" target="_blank" >https://ieeexplore.ieee.org/document/9214017</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1109/ICUAS48674.2020.9214017" target="_blank" >10.1109/ICUAS48674.2020.9214017</a>
Alternative languages
Result language
angličtina
Original language name
Controller design for highly maneuverable aircraft technology using structured singular value and direct search method
Original language description
The algebraic approach is applied to the HiMAT (Highly Maneuverable Aircraft Technology) control. The objective is to find a robust controller which guarantees robust stability and decoupled control of longitudinal model of a scaled remotely controlled vehicle version of the advanced fighter HiMAT. Control design is performed by decoupling the nominal multi-input multi-output system into two identical single-input single-output plants which are approximated by a 4th order transfer function. The algebraic approach is then used for pole placement design and the nominal closed-loop poles are tuned so that the peak of the μ-function is minimal. As an optimization tool, evolutionary algorithm Differential Migration is used in order to overcome the multimodality of the cost function yielding simple controller with decoupling for nominal plant which is compared with the D-K iteration through simulations of standard longitudinal manoeuvres documenting decoupled control obtained from algebraic approach for nominal plant as well as worst case perturbation. © 2020 IEEE.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20205 - Automation and control systems
Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2020
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
ISBN
978-1-72814-277-7
ISSN
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e-ISSN
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Number of pages
5
Pages from-to
529-533
Publisher name
Institute of Electrical and Electronics Engineers Inc.
Place of publication
Piscataway, New Jersey
Event location
Athens
Event date
Sep 1, 2020
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
000612041300069