标题: 飞控辅助设计用之异常气相模型之建立及其程式库设计
The Modeling and Library Designing of Abnormal Wind for the Controller Design of Aircraft
作者: 陈世国
Chen, Shi-Kou
张隆国
Lon-Kou Chang
电控工程研究所
关键字: 气象模型;大气紊流;微暴雷雨;阵风;程式库;飞行模拟;modeling;atmospheric turbulence;microburst;gust wind;library designing;flight simulation
公开日期: 1996
摘要: 本论文研究之目的乃在于建立包括大气紊流及微暴雷雨的多种不同气流模
式的程式库,并配合修改AIAA所提供的飞机模型,使得AIAA的飞机模型能
够加入气流模式对飞机运动的影响。这个模拟系统将可应用于飞机的设计
改良及测试飞行控制器性能等用途。在本论文中所建立的气象气流模型可
分为三类,第一类为离散式的阵风模型,包括上升气流,下降气流,侧风
,逆风,以及顺风。第二类为大气紊流模型,我们以von Karman,Dryden
的频谱模型及涡流阵列等方式来建立其模型。第三类气象模型为微暴雷雨
模型,以及多环状涡流倾斜式的微暴雷雨模型。此外,我们也建立一个简
单的下降暴雷与模型以及由DFW机场的微暴雷雨记录所发展得到的两组模
型。我们以将上述的气流模型,以程式库的方式,提供使用者可轻易的于
其飞机模型程式中呼叫使用。在本论文中,我们以AIAA的飞机模型作为飞
行运动模拟的对象,并展现各气流模型对AIAA飞机的飞行影响的模拟结果

The objective of this thesis is to design the library
subroutines of wind models like turbulence,microburst,and many
other special winds.We also clearly propose the way to modify
the program of the jet-plane,which is proposed in AIAA,so that
the wind effects can be applied to the aviation process of AIAA
plane.Moreover,our design can be primarily used for testing the
designs of airplanes and their flight controllers.In this
thesis,we consider three types of abnormal winds and their
mathematical models.The first one is the discrete gust wind
model,including updraft,downdraft,head wind,tail wind,and side
wind.The second one is the atmospheric turbulence model.We use
the von Karman spectrum,Dryden spectrum,and a vortex array to
generate this type of wind models.The third one is the
microburst.We have built up five samples for this model:such as,
a simple downdraft model,a single ring vortex model,a multi-ring
tilt vortices model,and DFW microburst models which are provided
by the reconstruction of DL-191 and AA-539.We have generated a
set of library subroutines for implementing the wind models.For
verifying our design,we use AIAA plane as the example plane.The
wind effects to the plane have been computed and shown in this
thesis.
URI: http://140.113.39.130/cdrfb3/record/nctu/#NT850327025
http://hdl.handle.net/11536/61679
显示于类别:Thesis