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Description
  • &lt;!--[if gte mso 9]&gt; Normal 0 21 false false false MicrosoftInternetExplorer4 &lt;![endif]--&gt;&lt;!--[if gte mso 9]&gt; &lt;![endif]--&gt;&lt;!--[if gte mso 10]&gt; /* Style Definitions */ table.MsoNormalTable {mso-style-name:&quot;Normální tabulka&quot;; mso-tstyle-rowband-size:0; mso-tstyle-colband-size:0; mso-style-noshow:yes; mso-style-parent:&quot;&quot;; mso-padding-alt:0cm 5.4pt 0cm 5.4pt; mso-para-margin:0cm; mso-para-margin-bottom:.0001pt; mso-pagination:widow-orphan; font-size:10.0pt; font-family:&quot;Times New Roman&quot;; mso-ansi-language:#0400; mso-fareast-language:#0400; mso-bidi-language:#0400;} &lt;![endif]--&gt; <p>This paper discusses the design and simulation of the Total-X flight control concept. Total-X has been implemented into the flight control logic of a light aircraft's flight control system. This implementation has been subjected to numerous simulations using rapid prototyping and real-time simulation envi
  • &lt;!--[if gte mso 9]&gt; Normal 0 21 false false false MicrosoftInternetExplorer4 &lt;![endif]--&gt;&lt;!--[if gte mso 9]&gt; &lt;![endif]--&gt;&lt;!--[if gte mso 10]&gt; /* Style Definitions */ table.MsoNormalTable {mso-style-name:&quot;Normální tabulka&quot;; mso-tstyle-rowband-size:0; mso-tstyle-colband-size:0; mso-style-noshow:yes; mso-style-parent:&quot;&quot;; mso-padding-alt:0cm 5.4pt 0cm 5.4pt; mso-para-margin:0cm; mso-para-margin-bottom:.0001pt; mso-pagination:widow-orphan; font-size:10.0pt; font-family:&quot;Times New Roman&quot;; mso-ansi-language:#0400; mso-fareast-language:#0400; mso-bidi-language:#0400;} &lt;![endif]--&gt; <p>This paper discusses the design and simulation of the Total-X flight control concept. Total-X has been implemented into the flight control logic of a light aircraft's flight control system. This implementation has been subjected to numerous simulations using rapid prototyping and real-time simulation envi (en)
Title
  • Simulations of Total-X based flight control system for light aircraft
  • Simulations of Total-X based flight control system for light aircraft (en)
skos:prefLabel
  • Simulations of Total-X based flight control system for light aircraft
  • Simulations of Total-X based flight control system for light aircraft (en)
skos:notation
  • RIV/00216305:26230/10:PU90527!RIV11-MSM-26230___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MSM0021630528)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 287498
http://linked.open...ai/riv/idVysledku
  • RIV/00216305:26230/10:PU90527
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • flight control system, light aircraft, Total-X control system, noise reduction, fuel consumption (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [2A9CDA388EB8]
http://linked.open...v/mistoKonaniAkce
  • Bezmiechowa
http://linked.open...i/riv/mistoVydani
  • Bezmiechowa
http://linked.open...i/riv/nazevZdroje
  • Conference of Avionics
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Chudý, Peter
  • Rzucidlo, Pawel
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
http://linked.open...n/vavai/riv/zamer
number of pages
http://purl.org/ne...btex#hasPublisher
  • Rzesow University of Technology
https://schema.org/isbn
  • 978-83-7199-623-8
http://localhost/t...ganizacniJednotka
  • 26230
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