Development of Flight Simulation Software
碩士 === 國立成功大學 === 電機工程研究所 === 84 === Aircraft technology is one of the main aspects in our conutry technology development. The main prupose of this research is to establish a flight simulation software which can be used for aircraft dynamic...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
1996
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/34132339202146267707 |
| Summary: | 碩士 === 國立成功大學 === 電機工程研究所 === 84 === Aircraft technology is one of the main aspects in our conutry
technology development. The main prupose of this research is to
establish a flight simulation software which can be used for
aircraft dynamic and navigational simulation. The aircraft
dynamic simulation system includes the following parts: (1)
Integration of the nonlinear state equations.(2)Tabular form of
aerodynamic data and environment model. (3) Engine model and
control blocks (4) Designated pilot command.In addition, in
this research, we incorporate navigation in the simulation.
This simulation may be combined with the foregoing aircraft
dynamic simulation to construct an integrated navigational and
dynamic simulation. The simulation is developed using MATLAB
with SIMULINK programming language and has been correlated with
test data.
|
|---|