📄 airlibex.mdl
字号:
Name " Convair 880 "
Ports [3, 3, 0, 0, 0]
Position [315, 261, 370, 379]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[5.7729 36.5760 185.8061 155920 3321800 "
" 5518200 0 0 0 57154]"
CD_wind "[0.024 0.150 0 0 0]"
CL_wind "[0.347 4.8 7.5 0.19 0]"
Cm_body "[0.0 -0.650 -4.5 -0.570 0]"
CY_body "[0 -0.812 0 0 0 0.184]"
Cl_body "[0 -0.117 -0.312 0.153 -0.050 0.019]"
Cn_body "[0 0.129 -0.011 -0.165 0.008 -0.076]"
x0 "[100 0.032161 0 0 0 0 0 0.032161 0 0 0 6"
"0]"
Port {
PortNumber 1
Name "x"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 2
Name "xdot"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 3
Name "var"
TestPoint off
RTWStorageClass "Auto"
}
}
Block {
BlockType Reference
Name " F-104 Starfighter "
Ports [3, 3, 0, 0, 0]
Position [315, 41, 370, 159]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[2.926 6.6751 18.21 4881 79993 81349 "
" 0 0 0 7393.7]"
CD_wind "[0.048 0.384 0 0 0]"
CL_wind "[0.122 2.005 1.9 0.684 0]"
Cm_body "[-0.028 -1.308 -4.83 -1.6 0]"
CY_body "[0 -1.045 0 0 -0 0.087]"
Cl_body "[0 -0.093 -0.272 0.154 -0.0173 0.0"
"079]"
Cn_body "[0 0.242 -0.093 -0.649 -0.0025 -0.0"
"435]"
x0 "[100 0.333846 0 0 0 0 0 0.333846 0 0 0 6"
"0]"
Port {
PortNumber 1
Name "x"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 2
Name "xdot"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 3
Name "var"
TestPoint off
RTWStorageClass "Auto"
}
}
Block {
BlockType Reference
Name " F4 Phantom "
Ports [3, 3, 0, 0, 0]
Position [175, 41, 230, 159]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[4.8768 11.79576 49.23861 33895.4489 16"
"5680.954 189543.35 0 2982.7995 0 17690.1]"
CD_wind "[0.0205 0.3 0 0 -0.1]"
CL_wind "[0.1 3.75 1.8 0 0.4]"
Cm_body "[0.025 -0.4 -2.7 0 -0.58]"
CY_body "[0 -0.68 0 0 0.0160 0.095]"
Cl_body "[0 -0.16 -0.34 0.13 -0.013 0.008]"
Cn_body "[0 0.125 -0.036 -0.270 0.001 -0.0"
"66]"
x0 "[260 -0.00907902 0 0 0 0 0 -0.00907902 0 "
" 0 0 60]"
}
Block {
BlockType Reference
Name " IAI Pioneer "
Ports [3, 3, 0, 0, 0]
Position [585, 41, 640, 159]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[0.5486 5.1511 2.8261 47.2259 90.9483 111"
".4754 0 -6.6462 0 190.512]"
CD_wind "[0.060 0.430 0 0.0180 0]"
CL_wind "[0.385 4.78 8.05 0.401 0]"
Cm_body "[0.194 -2.12 -36.6 -1.76 0]"
CY_body "[0 -0.819 0 0 0.191 0]"
Cl_body "[0 -0.023 -0.450 0.265 -0.161 -0.00229"
"]"
Cn_body "[0 0.109 -0.110 -0.200 0.0200 -0.0917]"
x0 "[60 -0.0293682 0 0 0 0 0 -0.0293682 0 0 0"
" 60]"
Port {
PortNumber 1
Name "x"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 2
Name "xdot"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 3
Name "var"
TestPoint off
RTWStorageClass "Auto"
}
}
Block {
BlockType Reference
Name " Learjet 24 "
Ports [3, 3, 0, 0, 0]
Position [175, 261, 230, 379]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[2.1336 10.3632 21.3677 37963 25489 63"
"723 0 1762.6 0 5896.8]"
CD_wind "[0.0216 0.3 0 0 0]"
CL_wind "[0.130 5.840 4.7 0.46 0]"
Cm_body "[0.05 -0.64 -15.5 -1.24 0]"
CY_body "[0 -0.730 0.0 0.400 0.0 0.140]"
Cl_body "[0 -0.110 -0.450 0.160 -0.178 0.0"
"19]"
Cn_body "[0 0.127 -0.008 -0.200 0.020 -0.074]"
x0 "[100 0.0524554 0 0 0 0 0 0.0524554 0 0 0"
" 60]"
Port {
PortNumber 1
Name "x"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 2
Name "xdot"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 3
Name "var"
TestPoint off
RTWStorageClass "Auto"
}
}
Block {
BlockType Reference
Name " SIAI-Marchetti S-211 "
Ports [3, 3, 0, 0, 0]
Position [40, 261, 95, 379]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[1.6459 8.0162 12.6348 1084.7 6507.9 "
"7050.3 0 271.16 0 1814.4]"
CD_wind "[0.0205 0.12 0 0 0]"
CL_wind "[0.149 5.50 10.0 0.38 0]"
Cm_body "[-0.08 -0.24 -17.7 -0.88 0]"
CY_body "[0 -1.00 -0.140 0.61 0 0.0280]"
Cl_body "[0 -0.11 -0.39 0.28 -0.1 0.05]"
Cn_body "[0 0.17 0.09 -0.26 0.003 -0.120]"
x0 "[100 0.0215504 0 0 0 0 0 0.0215504 0 0 0"
" 60]"
Port {
PortNumber 1
Name "x"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 2
Name "xdot"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 3
Name "var"
TestPoint off
RTWStorageClass "Auto"
}
}
Block {
BlockType Reference
Name " X-15 "
Ports [3, 3, 0, 0, 0]
Position [450, 41, 505, 159]
DropShadow on
FontName "Arial"
SourceBlock "airlib/B747"
SourceType "General Nonlinear Aircraft Model"
GM1 "[3.13 6.8153 18.58 4948.7 108470 11118"
"0 0 800 0 14170]"
CD_wind "[0.095 0.6 0 0 0]"
CL_wind "[0 3.5 0 0.54 0]"
Cm_body "[0 -1.2 -6.2 -0.9 0]"
CY_body "[0 -1.4 0 0 0.05 0.45]"
Cl_body "[0 -0.01 -0.35 0.04 -0.06 0.012]"
Cn_body "[0 0.5 0 -1.5 -0.04 -0.3]"
x0 "[100 0.392538 0 0 0 0 0 0.392538 0 0 0 6"
"0]"
Port {
PortNumber 1
Name "x"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 2
Name "xdot"
TestPoint off
RTWStorageClass "Auto"
}
Port {
PortNumber 3
Name "var"
TestPoint off
RTWStorageClass "Auto"
}
}
Annotation {
Position [78, 205]
ForegroundColor "blue"
Text "Fx0=18045.51; \nde0=-1.71374e-4;\ndh0=-0.017"
"1382; "
}
Annotation {
Position [208, 205]
ForegroundColor "blue"
Text "Fx0=26027; \nde0=0; \ndh0"
"=0.0493648; "
}
Annotation {
Position [343, 205]
ForegroundColor "blue"
Text "Fx0=20681; \nde0=-0.290419;\ndh0=0; "
" "
}
Annotation {
Position [483, 205]
ForegroundColor "blue"
Text "Fx0=40476.7; \nde0=-0.523384;\ndh0=0; "
" "
}
Annotation {
Position [623, 205]
ForegroundColor "blue"
Text "Fx0=309.8742; \nde0=0.145603; \ndh0=0; "
" "
}
Annotation {
Position [73, 425]
ForegroundColor "blue"
Text "Fx0=1776.7; \nde0=-0.139322;\ndh0=0; "
" "
}
Annotation {
Position [208, 425]
ForegroundColor "blue"
Text "Fx0=4865.1; \nde0=0.0132488;\ndh0=0; "
" "
}
Annotation {
Position [348, 425]
ForegroundColor "blue"
Text "Fx0=32632; \nde0=-0.0366749;\ndh0=0; "
" "
}
Annotation {
Position [483, 425]
ForegroundColor "blue"
Text "Fx0=4195.5; \nde0=0.0287194;\ndh0=0; "
" "
}
Annotation {
Position [301, 765]
Text "The aerodynamic data are taken from the web sit"
"e \"http://www.aae.uiuc.edu/m-selig/apasim/Aircraft-uiuc.html\".\nThis is an "
"open project, so feel free to contribute in any way. Giampiero Campa, Feb 200"
"3 "
}
Annotation {
Position [73, 645]
ForegroundColor "blue"
Text "Fx0=2626; \nde0=0.0169793;\ndh0=0; "
" "
}
Annotation {
Position [208, 645]
ForegroundColor "blue"
Text "Fx0=2501,91; \nde0=0.0323893;\ndh0=0; "
" "
}
Annotation {
Position [348, 645]
ForegroundColor "blue"
Text "Fx0=4664.76; \nde0=0.0548662;\ndh0=0; "
" "
}
Annotation {
Position [483, 645]
ForegroundColor "blue"
Text "Fx0=5457.08; \nde0=0.0141948;\ndh0=0; "
" "
}
Annotation {
Position [391, 715]
ForegroundColor "red"
Text "The initial state x0 together with the shown in"
"put values for Fx, de and dh, form an airplane trim point. "
" \nThe trim points were c"
"alculated with the utility \"trimmod\" (available on the fileexchange site), "
"by using thrust, de, alpha , theta as trim variables \nand vdot=0, al"
"phadot=0, qdot=0, Hdot=0; as trim requirements. Note that the given trim poin"
"t does NOT usually coincide with the point in the flight \nenvelope in which "
"the given constant aerodynamic coefficients form the best approximation of th"
"e true nonlinear aerodynamic model of the aircraft. "
}
}
}
⌨️ 快捷键说明
复制代码
Ctrl + C
搜索代码
Ctrl + F
全屏模式
F11
切换主题
Ctrl + Shift + D
显示快捷键
?
增大字号
Ctrl + =
减小字号
Ctrl + -