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Description
  • The paper deals with prediction of airplane’s maneuverability in horizontal correct decelerated turn. Calculations are made by numerical integration of equations of motion, expressed as nonlinear differential equations of first order. Three different models are considered with intention of determining a best one, offering acceptable accuracy balanced with simplicity. The airplane is described by aerodynamic, weight and powerplant characteristics. Matlab-Simulink has been used for all calculations and Microsoft Excell for data export.
  • The paper deals with prediction of airplane’s maneuverability in horizontal correct decelerated turn. Calculations are made by numerical integration of equations of motion, expressed as nonlinear differential equations of first order. Three different models are considered with intention of determining a best one, offering acceptable accuracy balanced with simplicity. The airplane is described by aerodynamic, weight and powerplant characteristics. Matlab-Simulink has been used for all calculations and Microsoft Excell for data export. (en)
Title
  • Computer Simulation in Use of Airplane Sharp Turn Maneuverability Predictions
  • Computer Simulation in Use of Airplane Sharp Turn Maneuverability Predictions (en)
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  • Computer Simulation in Use of Airplane Sharp Turn Maneuverability Predictions
  • Computer Simulation in Use of Airplane Sharp Turn Maneuverability Predictions (en)
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  • RIV/60162694:G43__/13:00502094!RIV14-MSM-G43_____
http://linked.open...avai/riv/aktivita
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  • 66600
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  • RIV/60162694:G43__/13:00502094
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  • computer simulation; maneuverability; turn (en)
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  • [5C3451145EE2]
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  • Kmetík, Martin
  • Salga, Jaroslav
http://localhost/t...ganizacniJednotka
  • G43
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