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Description
  • This article deals with the application of mathematical methods of experimental identification for determining the transfer functions parameters of some avionics subsystems. For the first approach the dynamic subsystem is considered as single-input and single-output system. MATLAB software support is used to compute parameters of those transfer functions. Obtained results of experimental identification are demonstrated on several examples.
  • This article deals with the application of mathematical methods of experimental identification for determining the transfer functions parameters of some avionics subsystems. For the first approach the dynamic subsystem is considered as single-input and single-output system. MATLAB software support is used to compute parameters of those transfer functions. Obtained results of experimental identification are demonstrated on several examples. (en)
Title
  • Possibilities of Experimental Parameter Identification of Avionics Subsystems
  • Possibilities of Experimental Parameter Identification of Avionics Subsystems (en)
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  • Possibilities of Experimental Parameter Identification of Avionics Subsystems
  • Possibilities of Experimental Parameter Identification of Avionics Subsystems (en)
skos:notation
  • RIV/60162694:G43__/11:00449313!RIV12-MO0-G43_____
http://linked.open...avai/riv/aktivita
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  • I
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  • 221751
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  • RIV/60162694:G43__/11:00449313
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  • experimental identification; transfer function; MATLAB (en)
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  • [F31EB04602BC]
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  • Brno
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  • Brno
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  • ICMT´11 - International Conference on Military Technologies 2011
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  • Dub, Michal
  • Jalovecký, Rudolf
  • Bystřický, Radek
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  • Univerzita obrany
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  • 978-80-7231-787-5
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  • G43
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