[Csp-commits] APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k fm.xml,NONE,1.1 fm.xml.gz.bak,NONE,1.1 model.xml,NONE,1.1

[<mk...@us...>]

Update of /cvsroot/csp/APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k
In directory sc8-pr-cvs1:/tmp/cvs-serv13807/Data/XML/vehicles/aircraft/m2k

Added Files:
	fm.xml fm.xml.gz.bak model.xml 
Log Message:
cspsim initial

--- NEW FILE: fm.xml ---
<?xml version="1.0" standalone="no"?>

<!-- 

	Mirage 2000 aerodynamics model

	many parameters are estimates. 
	
-->

<Object class="AeroDynamics">

	<!-- Wing geometry -->
	<Real name="wing_span">9.13</Real>
	<Real name="wing_chord">4.5</Real>
	<Real name="wing_area">41.0</Real>

	<!-- Control surfaces min/max angles -->
	<Real name="de_max">25.0</Real>
	<Real name="de_min">-16.0</Real>
	<Real name="da_max">+17.5</Real>
	<Real name="da_min">-17.5</Real>
	<Real name="dr_max">+20.0</Real>
	<Real name="dr_min">-20.0</Real>

	<!-- A=0.9 10^4 kg m^2       A -F -E -->
	<!-- C=6.0 10^4 kg m^2  I = -F  B -D -->
	<!-- B=5.4 10^4 Kg m^2      -E -D  C -->
	<!-- E=1.8 10^3 kg m^2 -->

	<!-- Mass/Inertial properties -->
	<!-- max mass -->
	<!-- <Real name="Mass">17500.0</Real> -->
	<!-- interceptor mass with a central tank
	<Real name="mass">12000.0</Real> -->
	<!-- interceptor mass -->
	<!-- <Real name="Mass">7500.0</Real> -->

	<!--
	<Matrix name="inertia">
		20354.0        0.0    6785.0
		    0.0   135691.0       0.0
	         6785.0        0.0  135691.0
	</Matrix> -->

	<Real name="g_min">-3.0</Real>
	<Real name="g_max">9.0</Real>

	<!--
	<Real name="thrust_max">9700.0</Real> -->

	<!-- Drag Parameters cx0 = 2 *">0.074 / ( rc^0.2 ) ; Cx=Cx0+KiCz^2 Ki(trainee induite) 1/pi*AR -->
	<Real name="cd0">0.02</Real>
	<Real name="cd_a">0.3</Real>
	<Real name="cd_de">0.02</Real>

	<!-- Lift Parameters -->
	<Real name="stall_aoa">31.0</Real>
	<Real name="cl0">0.14</Real>
	<Real name="cl_a">4.2</Real>
	<Real name="cl_adot">1.29</Real>
	<Real name="cl_q">1.5</Real>
	<Real name="cl_de">0.4</Real>

	<!-- Pitch Moment Parameters -->
	<Real name="cm0">-0.02</Real>
	<Real name="cm_a">-0.02</Real>
	<Real name="cm_adot">-1.73</Real>
	<Real name="cm_q">-3.6</Real>
	<Real name="cm_de">0.3</Real>

	<!-- Side Force Parameters -->
	<Real name="cy_beta">-0.29</Real>
	<Real name="cy_p">0.11</Real>
	<Real name="cy_r">0.0</Real>
	<Real name="cy_da">0.0</Real>
	<Real name="cy_dr">-0.01</Real>

	<!-- Roll moment parameters -->
	<Real name="ci_beta">-0.1</Real>
	<Real name="ci_p">-0.3</Real>
	<Real name="ci_r">0.3</Real>
	<Real name="ci_da">0.2</Real>
	<Real name="ci_dr">-0.03</Real>

	<!-- Yaw Moment Parameters -->
	<Real name="cn_beta">0.3</Real>
	<Real name="cn_p">0.03</Real>
	<Real name="cn_r">-0.04</Real>
	<Real name="cn_da">0.03</Real>
	<Real name="cn_dr">0.08</Real>

</Object>


--- NEW FILE: fm.xml.gz.bak ---
(This appears to be a binary file; contents omitted.)

--- NEW FILE: model.xml ---
<?xml version="1.0" standalone="no"?>

<Object class="ObjectModel" static="1">
	<External name="model_path">Models/m2k2g.3ds</External>
	<Vector name="axis_0">1 0 0</Vector>
	<Vector name="axis_1">0 1 0</Vector>
	<Matrix name="rotation">1 0 0 0 1 0 0 0 1</Matrix>
	<Real name="scale">1.0</Real>
</Object>