[Csp-commits] APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k gear.xml,NONE,1.1 thrust.xml,NONE,1.1

[<de...@us...>]

Update of /cvsroot/csp/APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k
In directory sc8-pr-cvs1:/tmp/cvs-serv4952

Added Files:
	gear.xml thrust.xml 
Log Message:
no message

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

<!-- 
    Mirage 2000 gear
-->


        
<Object class="GearDynamics" name="gear_dynamics">
	<List name="gear_set">
        <!-- all of these values are complete guesses for testing only! -->
                <Object class="LandingGear"> <!-- nosewheel -->
                    <Vector name="max_position">0.0 4.75 -2.0</Vector>
                    <Vector name="motion">0 0 1.0</Vector>
                    <Real name="damage_limit">80000.0:10000.0</Real>
                    <Float name="compression_limit">0.5</Float>
                    <Float name="K">200000.0</Float>
                    <Float name="beta">10000.0</Float>
                    <Float name="brake_limit">3000.0</Float>
                    <Float name="static_friction">0.7</Float>
                    <Float name="dynamic_friction">0.5</Float>
                    <Float name="steering_limit">45.0</Float>
                    <Float name="tire_K">200000.0</Float>
                </Object>
                <Object class="LandingGear"> <!-- left main -->
                    <Vector name="max_position">-1.75 -0.7 -2.0</Vector>
                    <Vector name="motion">0 0 1.0</Vector>
                    <Real name="damage_limit">80000.0</Real>
                    <Float name="compression_limit">0.5</Float>
                    <Float name="K">300000.0</Float>
                    <Float name="beta">10000.0</Float>
                    <Float name="brake_limit">3000.0</Float>
                    <Float name="static_friction">0.7</Float>
                    <Float name="dynamic_friction">0.5</Float>
                    <Float name="tire_K">200000.0</Float>
                </Object>
                <Object class="LandingGear"> <!-- right main -->
                    <Vector name="max_position">1.75 -0.7 -2.0</Vector>
                    <Vector name="motion">0 0 1.0</Vector>
                    <Real name="damage_limit">80000.0:10000.0</Real>
                    <Float name="compression_limit">0.5</Float>
                    <Float name="K">300000.0</Float>
                    <Float name="beta">10000.0</Float>
                    <Float name="brake_limit">3000.0</Float>
                    <Float name="static_friction">0.7</Float>
                    <Float name="dynamic_friction">0.5</Float>
                    <Float name="tire_K">200000.0</Float>
                </Object>
	</List>
</Object>
    
    

--- NEW FILE: thrust.xml ---
<!-- 

Extracted from F4/SP3: f16cj.dat

NOTE: double check that XBreaks and YBreaks are
     correct... I may have reversed these.  X is altitude
     in meters, Y is mach number.

-->

<Object class="ThrustData" static="1">
    <Table name='idle_thrust'>
        <XBreaks spacing='1000.0'>
            0.0 3048.0 6096.0 9144.0 12192.0 15240.0 18288.0 30480.0
        </XBreaks>
        <YBreaks spacing='0.1'>
            0.0 0.2 0.4 0.6 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2
        </YBreaks>
        <Values>
            363.6 288.6075 27.27 -463.59 -1227.15 -1749.825 -1636.2 136.35 2272.5 3954.15 4761.342 4368.654 3926.88 3436.02 2932.8885 2405.214 1840.725 1276.236 736.29
            277.245 193.1625 11.3625 -322.695 -863.55 -965.8125 -636.3 795.375 2454.3 3681.45 4272.3 4104.135 3865.5225 3579.1875 3245.13 2863.35 2481.57 2004.345 1574.8425
            359.055 313.605 156.8025 -136.35 -590.85 -636.3 -270.4275 931.725 2272.5 3386.025 3999.6 4025.961 4025.961 4025.961 4021.416 3979.1475 3932.334 3885.5205 3838.707
            527.22 459.045 343.1475 159.075 -112.2615 -295.425 -155.439 772.65 1954.35 2999.7 3726.9 4067.775 4408.65 4726.8 5113.125 5499.45 5908.5 6340.275 6817.5
            663.57 604.485 513.585 413.595 272.7 -11.3625 -90.9 454.5 1318.05 2090.7 2658.825 2972.43 3269.673 3566.916 3817.8 3999.6 4067.775 4056.867 3986.874
            818.1 772.65 693.1125 618.12 499.95 363.6 318.15 681.75 1181.7 1704.375 2079.3375 2317.95 2420.2125 2448.3915 2462.0265 2462.0265 2462.0265 2448.3915 2378.3985
            409.05 386.325 346.7835 309.06 249.975 181.8 159.075 340.875 590.85 852.1875 1039.896 1158.975 1209.879 1223.9685 1231.2405 1231.2405 1231.2405 1223.9685 1188.972
            25.452 24.0885 21.816 19.5435 15.453 11.3625 9.999 21.3615 36.8145 53.1765 64.9935 72.2655 75.447 76.356 76.8105 76.8105 76.8105 76.356 74.538
        </Values>
    </Table>
    <Table name='mil_thrust'>
        <XBreaks spacing='1000.0'>
            0.0 3048.0 6096.0 9144.0 12192.0 15240.0 18288.0 30480.0
        </XBreaks>
        <YBreaks spacing='0.1'>
            0.0 0.2 0.4 0.6 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2
        </YBreaks>
        <Values>
            6344.3655 6223.923 6189.8355 6204.3795 6317.55 6363.0 6340.275 6067.575 5658.525 5181.3 4761.342 4368.654 3926.88 3436.02 2932.8885 2405.214 1840.725 1276.236 736.29
            4533.6375 4366.836 4444.101 4695.894 4867.695 4867.695 4819.9725 4772.25 4676.805 4510.0035 4319.1135 4104.135 3865.5225 3579.1875 3245.13 2863.35 2481.57 2004.345 1574.8425
            3089.691 2955.159 3094.236 3319.2135 3628.2735 3721.9005 3756.897 3850.524 3932.334 3979.1475 4021.416 4025.961 4025.961 4025.961 4021.416 3979.1475 3932.334 3885.5205 3838.707
            1863.45 1836.18 1949.805 2117.97 2417.94 2579.2875 2772.45 2999.7 3226.95 3499.65 3772.35 4067.775 4408.65 4726.8 5113.125 5499.45 5908.5 6340.275 6817.5
            1263.51 1223.514 1288.053 1407.132 1610.2935 1733.9175 1882.539 2056.158 2254.32 2477.025 2675.187 2972.43 3269.673 3566.916 3817.8 3999.6 4067.775 4056.867 3986.874
            825.8265 811.2825 904.0005 962.1765 1118.5245 1217.151 1338.5025 1477.5795 1651.653 1854.36 2086.155 2317.95 2420.2125 2448.3915 2462.0265 2462.0265 2462.0265 2448.3915 2378.3985
            412.686 405.8685 452.2275 480.861 559.035 608.5755 669.4785 739.017 825.8265 927.18 1043.0775 1158.975 1209.879 1223.9685 1231.2405 1231.2405 1231.2405 1223.9685 1188.972
            25.9065 25.452 28.179 29.997 34.9965 38.178 41.814 46.359 51.813 58.176 64.9935 72.2655 75.447 76.356 76.8105 76.8105 76.8105 76.356 74.538
        </Values>
    </Table>
    <Table name='ab_thrust'>
        <XBreaks spacing='1000.0'>
            0.0 3048.0 6096.0 9144.0 12192.0 15240.0 18288.0 30480.0
        </XBreaks>
        <YBreaks spacing='0.1'>
            0.0 0.2 0.4 0.6 0.8 0.9 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2
        </YBreaks>
        <Values>
            10226.25 9735.39 10317.15 11017.08 11848.815 12498.75 13128.687 14316.75 15225.75 15453.0 15680.25 15680.25 15680.25 15453.0 15112.125 14771.25 14203.125 13635.0 13180.5
            7272.0 7135.65 7662.87 8594.595 9578.5875 9999.0 10598.4855 11817.0 12953.25 13635.0 14089.5 14203.125 14089.5 13862.25 13521.375 13180.5 12839.625 12385.125 11817.0
            5226.75 5101.7625 5567.625 6253.92 7260.6375 7726.5 8317.35 9203.625 9999.0 10680.75 11135.25 11362.5 11476.125 11476.125 11476.125 11362.5 11248.875 10908.0 10453.5
            3329.2125 3328.3035 3705.993 4220.0325 5051.7675 5567.625 6128.478 6931.125 7726.5 8408.25 8862.75 9203.625 9317.25 9317.25 9317.25 9203.625 8976.375 8749.125 8635.5
            2011.1625 2015.7075 2272.5 2590.65 3117.87 3522.375 3927.789 4658.625 5340.375 5908.5 6249.375 6590.25 6703.875 6817.5 6817.5 6817.5 6703.875 6590.25 6476.625
            1181.7 1181.7 1288.5075 1461.2175 1795.275 2045.25 2298.4065 2727.0 3181.5 3522.375 3749.625 3863.25 3931.425 3976.875 3999.6 3999.6 3999.6 3976.875 3863.25
            590.85 590.85 644.481 730.836 897.6375 1022.625 1149.4305 1363.5 1590.75 1761.1875 1874.8125 1931.625 1965.7125 1988.4375 1999.8 1999.8 1999.8 1988.4375 1931.625
            74.0835 74.0835 80.4465 91.3545 112.2615 127.7145 143.622 170.4375 199.071 219.978 234.522 241.3395 245.8845 248.6115 249.975 249.975 249.975 248.6115 241.3395
        </Values>
    </Table>
</Object>