Simulation and Prototyping of FCS for Sport Aircraft
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26230%2F13%3APU106421" target="_blank" >RIV/00216305:26230/13:PU106421 - isvavai.cz</a>
Result on the web
<a href="http://www.emeraldinsight.com/journals.htm?articleid=17097834" target="_blank" >http://www.emeraldinsight.com/journals.htm?articleid=17097834</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1108/AEAT-10-2012-0186" target="_blank" >10.1108/AEAT-10-2012-0186</a>
Alternative languages
Result language
angličtina
Original language name
Simulation and Prototyping of FCS for Sport Aircraft
Original language description
The workload experienced by the pilots while operating and navigating an airplane in areas with dense air traffic, magnified by the complexity of meteorological phenomena and physiological limitations of manned flight support the rationality of a pilot workload reducing system. As LSAs (Light Sport Aircraft) are mostly flown by a single pilot, their operational concept would benefit from an intelligent flight control system assisting in aircrafts safe operation. This opinion motivated the authors to an experimental implementation of assisting flight control strategies. Proposed flight control concept for LSA integrates mechanical and digital control systems in a synergic way, allowing flight safety and comfort improvements by maintaining or augmenting overall system reliability and improving user experience in manual flying. The concept of an assisting flight control system is an intermediate step between manual and fly-by-wire control, making it a viable option for installations on board of price sensitive light sport aircraft. Presented paper describes the simulation and prototyping of control algorithms for an assisting flight control and navigation system. The applied control strategy uses classical control theory along with implementation of flight envelope protection features. The proposed flight control system was subjected to real-time and pilot-in-the-loop experiments in a light aircraft simulation lab SimStar.
Czech name
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Czech description
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Classification
Type
J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database
CEP classification
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OECD FORD branch
20206 - Computer hardware and architecture
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
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Aircraft Engineering and Aerospace Technology: An International Journal
ISSN
0002-2667
e-ISSN
—
Volume of the periodical
2013
Issue of the periodical within the volume
85
Country of publishing house
GB - UNITED KINGDOM
Number of pages
15
Pages from-to
400-415
UT code for WoS article
000326668300006
EID of the result in the Scopus database
2-s2.0-84884873528