airdata2.htm

来自「MATLAB在飞行动力学和控制中应用的工具」· HTM 代码 · 共 40 行

HTM
40 行
字号 
<HTML>
<HEAD>
<TITLE>FDC help: Airdata2</TITLE>
</HEAD>
<BODY BGCOLOR="#DED6D3" TEXT="#000000" LINK="#660033" VLINK="#660033" ALINK="#000080">
<H2>Subsystem <I><FONT FACE="Arial","Helvetica","Sans Serif">Airdata2</FONT></I></H2>

<I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif">Airdata2</FONT></I> is a masked S<SMALL>IMULINK</SMALL> subsystem, used to compute the impact pressure <I>q<SUB>c</SUB></I>, equivalent airspeed <I>V<SUB>e</SUB></I>, and the calibrated airspeed <I>V<SUB>c</SUB></I>. The block <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif">Airdata2</FONT></I> is contained in the subsystem <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif"><A HREF="adgrp.htm">Airdata Group</A></FONT></I> of the system <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif"><A HREF="beaver.htm">Beaver</A></FONT></I>. Other airdata
(-related) variables are computed in the blocks <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif"><A HREF="atmosph.htm">Atmosph</A></FONT></I>, <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif"><A HREF="airdata1.htm">Airdata1</A></FONT></I>, and <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif"><A HREF="airdata3.htm">Airdata3</A></FONT></I>, which also contained in the subsystem <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif"><I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif">Airdata Group</FONT></I></FONT></I>.

<H3>Inputvectors: <I>yatm</I> and <I>yad1</I></H3>
<PRE>  yatm = [rho ps T mu g]'   (atmospheric properties, computed in
                                               the block <A HREF="atmosph.htm">Atmosph</A>)
  yad1 = [a M qdyn]',      (speed of sound, Mach number, dynamic
                        pressure, computed in the block <A HREF="airdata1.htm">Airdata1</A>)

 {rho  : airdensity [kg/m^3]                                    }
  ps   : static pressure [N/m^2]
 {T    : temperature [K]                                        }
 {mu   : dynamic viscosity [kg/(m*s)]                           }
 {g    : acceleration of gravity [m/s^2]                        }

 {a    : speed of sound [m/s]                                   }
  M    : Mach number [-]
  qdyn : dynamic pressure [N/m^2]
</PRE>
The inputvariables which are not actually used by <I><FONT SIZE=2 FACE="Arial","Helvetica","Sans Serif">Airdata2</FONT></I> have been displayed between accolades.

<H3>Outputvector: <I>yad2</I></H3>
<PRE>  yad2 = [qc Ve Vc]'

  qc   : impact pressure [N/m^2]
  Ve   : equivalent airspeed [m/s]
  Vc   : calibrated airspeed [m/s]
</PRE>

</BODY>

</HTML>

airdata2.htm - 源码说明

本页面展示了「MATLAB在飞行动力学和控制中应用的工具」中的 airdata2.htm 源码文件，采用 HTM 编程语言编写，共 40 行代码。您可以在线阅读完整代码内容，也可以返回资源详情页下载完整源码包进行本地学习和开发。

虫虫开发者社区收录了大量与Matlab相关的技术资源，包括源代码、技术文档、电路图等，是电子工程师和嵌入式开发者的专业学习平台。

⌨️ 快捷键说明

复制代码Ctrl + C
搜索代码Ctrl + F
全屏模式F11
增大字号Ctrl + =
减小字号Ctrl + -
显示快捷键?