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Modellering av vind och turbulens för en High-Fidelity flygsimuleringsmodell

Praceus, Julian (2013) In ISSN 0280-5316
Department of Automatic Control
Abstract
The aim of this thesis is to develop a model which simulates the dynamic atmosphere as well as the implementation of this model with Matlab/Simulink. The dynamic atmosphere contains the characteristics of wind, turbulence, wind gusts and wind shear, which is integrated in a high fidelity flight simulation model where the dynamics of an aircraft in the atmosphere will be simulated. After the description of the physical characteristics of the dynamic atmosphere, these characteristics are reflected – in a simplified form - by the model.

The model is based on the Military Specification MIL-F-8785C of the US Department of Defense which contains established functions for the behavior of turbulence, wind gusts and wind shear. These functions... (More)
The aim of this thesis is to develop a model which simulates the dynamic atmosphere as well as the implementation of this model with Matlab/Simulink. The dynamic atmosphere contains the characteristics of wind, turbulence, wind gusts and wind shear, which is integrated in a high fidelity flight simulation model where the dynamics of an aircraft in the atmosphere will be simulated. After the description of the physical characteristics of the dynamic atmosphere, these characteristics are reflected – in a simplified form - by the model.

The model is based on the Military Specification MIL-F-8785C of the US Department of Defense which contains established functions for the behavior of turbulence, wind gusts and wind shear. These functions are transformed to suitable algorithms to meet the compliance with the Institute of Flight System Dynamics at the TU Munich. Finally the
programed Simulink-module is thoroughly verified to ensure a realistic and reliable application in flight simulations. (Less)
Please use this url to cite or link to this publication:
author
Praceus, Julian
supervisor
organization
year
type
H3 - Professional qualifications (4 Years - )
subject
publication/series
ISSN 0280-5316
other publication id
ISRN LUTFD2/TFRT--5922--SE
language
Swedish
additional info
month=july
id
3971234
date added to LUP
2013-08-17 12:31:38
date last changed
2013-08-17 12:31:38
@misc{3971234,
  abstract     = {{The aim of this thesis is to develop a model which simulates the dynamic atmosphere as well as the implementation of this model with Matlab/Simulink. The dynamic atmosphere contains the characteristics of wind, turbulence, wind gusts and wind shear, which is integrated in a high fidelity flight simulation model where the dynamics of an aircraft in the atmosphere will be simulated. After the description of the physical characteristics of the dynamic atmosphere, these characteristics are reflected – in a simplified form - by the model.

The model is based on the Military Specification MIL-F-8785C of the US Department of Defense which contains established functions for the behavior of turbulence, wind gusts and wind shear. These functions are transformed to suitable algorithms to meet the compliance with the Institute of Flight System Dynamics at the TU Munich. Finally the
programed Simulink-module is thoroughly verified to ensure a realistic and reliable application in flight simulations.}},
  author       = {{Praceus, Julian}},
  language     = {{swe}},
  note         = {{Student Paper}},
  series       = {{ISSN 0280-5316}},
  title        = {{Modellering av vind och turbulens för en High-Fidelity flygsimuleringsmodell}},
  year         = {{2013}},
}