Measures and lmis for validation of an aircraft with mrac and uncertain actuator dynamics
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F21%3A00347991" target="_blank" >RIV/68407700:21230/21:00347991 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Measures and lmis for validation of an aircraft with mrac and uncertain actuator dynamics
Original language description
It is well known that actuator dynamics with degraded performance can lead to poor stability and tracking for adaptive control. In this paper, we use occupation measures and LMI relaxations (called the moment sums of squares or Lasserre hierarchy) for verification and validation of a longitudinal F-16 aircraft model with MRAC and higher order actuator dynamics with uncertain parameters and deflection saturation. These uncertain parameters are represented explicitly in the space of occupation measures. To improve numerical scalability, we exploit sparsity for ordinary differential equations (ODEs) using parsimony to partition the dynamics. We finally compare these main results to those obtained using Monte-Carlo methods.
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
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
AIAA Scitech 2021 Forum
ISBN
978-1-62410-609-5
ISSN
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e-ISSN
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Number of pages
8
Pages from-to
1-8
Publisher name
American Institute of Aeronautics and Astronautics
Place of publication
Reston
Event location
Reston
Event date
Jan 11, 2021
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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