Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts
This thesis provides background, theory, and examples for a high performance fighter aircraft (a modified model of F-16) control design. There are mainly three parts in this thesis. The first part presents the development of a software package for flight simulation of a high performance fighter airc...
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sg-ntu-dr.10356-196032023-07-04T15:38:31Z Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts Zhang, Wei Qiang Wang, Jianliang School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation This thesis provides background, theory, and examples for a high performance fighter aircraft (a modified model of F-16) control design. There are mainly three parts in this thesis. The first part presents the development of a software package for flight simulation of a high performance fighter aircraft (a modified model of F-16). The package is developed using MATLAB\SIMULINK. It consists of one SIMULINK model for simulation, one SIMULINK model for trimming/linearization and some essential functions. In this part, an overview of aircraft equations of motion is demonstrated to provide a basic understanding of flight dynamics. The fully nonlinear aircraft model is used with the six-degree-of-freedom (6-DOF) equations of motion. Some additional nonlinear aircraft dynamics such as actuator saturation, auto-scheduled leading-edge flaps and engine model are also included. C MEX-files are programmed to compute aero-dynamic coefficients and engine thrust. This makes the software package more effective and efficient in flight simulation and flight dynamic analysis. The package is also a reliable and flexible tool for checking control design methodology in the next two parts. Master of Engineering 2009-12-14T06:17:38Z 2009-12-14T06:17:38Z 1997 1997 Thesis http://hdl.handle.net/10356/19603 en Nanyang Technological University 168 p. application/pdf |
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DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation Zhang, Wei Qiang Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts |
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This thesis provides background, theory, and examples for a high performance fighter aircraft (a modified model of F-16) control design. There are mainly three parts in this thesis. The first part presents the development of a software package for flight simulation of a high performance fighter aircraft (a modified model of F-16). The package is developed using MATLAB\SIMULINK. It consists of one SIMULINK model for simulation, one SIMULINK model for trimming/linearization and some essential functions. In this part, an overview of aircraft equations of motion is demonstrated to provide a basic understanding of flight dynamics. The fully nonlinear aircraft model is used with the six-degree-of-freedom (6-DOF) equations of motion. Some additional nonlinear aircraft dynamics such as actuator saturation, auto-scheduled leading-edge flaps and engine model are also included. C MEX-files are programmed to compute aero-dynamic coefficients and engine thrust. This makes the software package more effective and efficient in flight simulation and flight dynamic analysis. The package is also a reliable and flexible tool for checking control design methodology in the next two parts. |
author2 |
Wang, Jianliang |
author_facet |
Wang, Jianliang Zhang, Wei Qiang |
format |
Theses and Dissertations |
author |
Zhang, Wei Qiang |
author_sort |
Zhang, Wei Qiang |
title |
Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts |
title_short |
Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts |
title_full |
Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts |
title_fullStr |
Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts |
title_full_unstemmed |
Control of a high performance fighter aircraft by using H(infinity) theory and neural-fuzzy concepts |
title_sort |
control of a high performance fighter aircraft by using h(infinity) theory and neural-fuzzy concepts |
publishDate |
2009 |
url |
http://hdl.handle.net/10356/19603 |
_version_ |
1772825907379044352 |