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[Csp-commits] APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k thrust.xml,1.1,1.2
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From: <mk...@us...> - 2003-06-20 17:45:51
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Update of /cvsroot/csp/APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k
In directory sc8-pr-cvs1:/tmp/cvs-serv31201
Modified Files:
thrust.xml
Log Message:
fixed thrust units and x,y ordering
Index: thrust.xml
===================================================================
RCS file: /cvsroot/csp/APPLICATIONS/CSPSim/Data/XML/vehicles/aircraft/m2k/thrust.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -C2 -d -r1.1 -r1.2
*** thrust.xml 19 Jun 2003 19:32:36 -0000 1.1
--- thrust.xml 20 Jun 2003 17:45:48 -0000 1.2
***************
*** 11,65 ****
<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>
--- 11,65 ----
<Object class="ThrustData" static="1">
<Table name='idle_thrust'>
! <XBreaks 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
+ </XBreaks>
+ <YBreaks spacing='1000.0'>
+ 0.0 3048.0 6096.0 9144.0 12192.0 15240.0 18288.0 30480.0
</YBreaks>
<Values>
! 3636.0 2886.075 272.7 -4635.9 -12271.5 -17498.25 -16362.0 1363.5 22725.0 39541.5 47613.42 43686.54 39268.8 34360.2 29328.885 24052.14 18407.25 12762.36 7362.9
! 2772.45 1931.625 113.625 -3226.95 -8635.5 -9658.125 -6363.0 7953.75 24543.0 36814.5 42723.0 41041.35 38655.225 35791.875 32451.3 28633.5 24815.7 20043.45 15748.425
! 3590.55 3136.05 1568.025 -1363.5 -5908.5 -6363.0 -2704.275 9317.25 22725.0 33860.25 39996.0 40259.61 40259.61 40259.61 40214.16 39791.475 39323.34 38855.205 38387.07
! 5272.2 4590.45 3431.475 1590.75 -1122.615 -2954.25 -1554.39 7726.5 19543.5 29997.0 37269.0 40677.75 44086.5 47268.0 51131.25 54994.5 59085.0 63402.75 68175.0
! 6635.7 6044.85 5135.85 4135.95 2727.0 -113.625 -909.0 4545.0 13180.5 20907.0 26588.25 29724.3 32696.73 35669.16 38178.0 39996.0 40677.75 40568.67 39868.74
! 8181.0 7726.5 6931.125 6181.2 4999.5 3636.0 3181.5 6817.5 11817.0 17043.75 20793.375 23179.5 24202.125 24483.915 24620.265 24620.265 24620.265 24483.915 23783.985
! 4090.5 3863.25 3467.835 3090.6 2499.75 1818.0 1590.75 3408.75 5908.5 8521.875 10398.96 11589.75 12098.79 12239.685 12312.405 12312.405 12312.405 12239.685 11889.72
! 254.52 240.885 218.16 195.435 154.53 113.625 99.99 213.615 368.145 531.765 649.935 722.655 754.47 763.56 768.105 768.105 768.105 763.56 745.38
</Values>
</Table>
<Table name='mil_thrust'>
! <XBreaks 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
+ </XBreaks>
+ <YBreaks spacing='1000.0'>
+ 0.0 3048.0 6096.0 9144.0 12192.0 15240.0 18288.0 30480.0
</YBreaks>
<Values>
! 63443.655 62239.23 61898.355 62043.795 63175.5 63630.0 63402.75 60675.75 56585.25 51813.0 47613.42 43686.54 39268.8 34360.2 29328.885 24052.14 18407.25 12762.36 7362.9
! 45336.375 43668.36 44441.01 46958.94 48676.95 48676.95 48199.725 47722.5 46768.05 45100.035 43191.135 41041.35 38655.225 35791.875 32451.3 28633.5 24815.7 20043.45 15748.425
! 30896.91 29551.59 30942.36 33192.135 36282.735 37219.005 37568.97 38505.24 39323.34 39791.475 40214.16 40259.61 40259.61 40259.61 40214.16 39791.475 39323.34 38855.205 38387.07
! 18634.5 18361.8 19498.05 21179.7 24179.4 25792.875 27724.5 29997.0 32269.5 34996.5 37723.5 40677.75 44086.5 47268.0 51131.25 54994.5 59085.0 63402.75 68175.0
! 12635.1 12235.14 12880.53 14071.32 16102.935 17339.175 18825.39 20561.58 22543.2 24770.25 26751.87 29724.3 32696.73 35669.16 38178.0 39996.0 40677.75 40568.67 39868.74
! 8258.265 8112.825 9040.005 9621.765 11185.245 12171.51 13385.025 14775.795 16516.53 18543.6 20861.55 23179.5 24202.125 24483.915 24620.265 24620.265 24620.265 24483.915 23783.985
! 4126.86 4058.685 4522.275 4808.61 5590.35 6085.755 6694.785 7390.17 8258.265 9271.8 10430.775 11589.75 12098.79 12239.685 12312.405 12312.405 12312.405 12239.685 11889.72
! 259.065 254.52 281.79 299.97 349.965 381.78 418.14 463.59 518.13 581.76 649.935 722.655 754.47 763.56 768.105 768.105 768.105 763.56 745.38
</Values>
</Table>
<Table name='ab_thrust'>
! <XBreaks 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
+ </XBreaks>
+ <YBreaks spacing='1000.0'>
+ 0.0 3048.0 6096.0 9144.0 12192.0 15240.0 18288.0 30480.0
</YBreaks>
<Values>
! 102262.5 97353.9 103171.5 110170.8 118488.15 124987.5 131286.87 143167.5 152257.5 154530.0 156802.5 156802.5 156802.5 154530.0 151121.25 147712.5 142031.25 136350.0 131805.0
! 72720.0 71356.5 76628.7 85945.95 95785.875 99990.0 105984.855 118170.0 129532.5 136350.0 140895.0 142031.25 140895.0 138622.5 135213.75 131805.0 128396.25 123851.25 118170.0
! 52267.5 51017.625 55676.25 62539.2 72606.375 77265.0 83173.5 92036.25 99990.0 106807.5 111352.5 113625.0 114761.25 114761.25 114761.25 113625.0 112488.75 109080.0 104535.0
! 33292.125 33283.035 37059.93 42200.325 50517.675 55676.25 61284.78 69311.25 77265.0 84082.5 88627.5 92036.25 93172.5 93172.5 93172.5 92036.25 89763.75 87491.25 86355.0
! 20111.625 20157.075 22725.0 25906.5 31178.7 35223.75 39277.89 46586.25 53403.75 59085.0 62493.75 65902.5 67038.75 68175.0 68175.0 68175.0 67038.75 65902.5 64766.25
! 11817.0 11817.0 12885.075 14612.175 17952.75 20452.5 22984.065 27270.0 31815.0 35223.75 37496.25 38632.5 39314.25 39768.75 39996.0 39996.0 39996.0 39768.75 38632.5
! 5908.5 5908.5 6444.81 7308.36 8976.375 10226.25 11494.305 13635.0 15907.5 17611.875 18748.125 19316.25 19657.125 19884.375 19998.0 19998.0 19998.0 19884.375 19316.25
! 740.835 740.835 804.465 913.545 1122.615 1277.145 1436.22 1704.375 1990.71 2199.78 2345.22 2413.395 2458.845 2486.115 2499.75 2499.75 2499.75 2486.115 2413.395
</Values>
</Table>
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