<?xml version="1.0" encoding="UTF-8" ?>
<CT:data version="1.00" xmlns:CT="http://www.adobri.com/tra">
<CT:section name="TraInfo">

<!-- starting date (1 jan 2000) = 2451544.5JD 
    2001 == 2451910.5 2002 =  2452275.5 2003 == 2452640.5 2004 == 2453005.5
    2005 == 2453371.5 2006 == 2453736.5 2007 == 2454101.5 2008 == 2454466.5
    2009 == 2454832.5 2010 == 2455197.5 2011 == 2455562.5 2012 == 2455927.5
    2013 == 2456293.5 2014 == 2456658.5 2015 == 2457023.5 
    or set as in keplers epoch: 11291.79166666
    or set as normal date and time DD/MM/YY HH:MM:SS:MLS-->
    <CT:setting name="dStartJD0" value="2451544.5" />
    <CT:setting name="dStartSecond" value="2451544.5" />
    <CT:setting name="dStartJD0" value="2455625.1696833" />
    <CT:setting name="dStartJD" value="11291.79166666" />
    <CT:setting name="dStartJD0" value="11291.854004622962962962962962963" />
    <CT:setting name="dStartJD0" value="11292.79166666" />

    <CT:setting name="RGBImageW" value="1280" />
    <CT:setting name="RGBImageH" value="720" />
<!-- int iProfile = 0; 
              // 0 == XY , 1 == YZ, 2 == XZ 3 == -YZ 4 == -XZ 5==-XY
              // 0 or XY is a view from North to south, 5 (- XY) is a view from south to north
              // 1 or YZ is a view to easter -->
    <CT:setting name="RGBView" value="0" />
<!--  EARTH 2 MOON  9 -->

    <CT:setting name="RGBReferenceBody" value="2" />
<!-- max amount of pictures -->
    <CT:setting name="RGBMaxPictures" value="1024" />
<!-- one picture per sec -->
    <CT:setting name="RGBSecPerPictures" value="8640" />
<!-- scale in m -->
    <CT:setting name="RGBScale" value="90000000" />

    <CT:setting name="IterPerSec" value="128" />
    <CT:setting name="StartLandingIteraPerSec" value="772050" />
<!-- next vaue actualy just a reference it will be used in-->
<!-- GMMoon = MoonM * GBig and GMEarth = EarthM*GBig      -->
<!-- know GMMoon and GMEarth will give proper value for M -->
    <CT:setting name="Gbig" value="6.6742799999999995e-011" />
    <CT:setting name="TotalDays0" value="1" />
    <CT:setting name="TotalDays" value="0.062337962962962962962962962962963" />

    <CT:setting name="EarthCurTime" value="11036.971719672511" />
    <CT:setting name="AU" value="149597870697.39999" />
    <CT:setting name="ProbM0" value="67.5" />
    <CT:setting name="ProbM" value="1.0" />
    <CT:setting name="ProbKeplerLine1" value="ISS (ZARYA)" />
    <CT:setting name="@ProbKeplerLine2" value="1 25544U 98067A   11062.66968330  .00024457  00000-0  18183-3 0  9357" />
    <CT:setting name="@ProbKeplerLine3" value="2 25544 051.6480 342.0829 0005279 039.9625 033.1957 15.72669582704292" />
    <CT:setting name="@ProbKeplerLine2" value="1 25544U 98067A   11291.79166666  .00024457  00000-0  18183-3 0  9357" />
    <CT:setting name="@ProbKeplerLine3" value="2 25544 051.6480 342.0829 0005279 039.9625 033.1957 15.72669582704292" />

     <CT:setting name="ProbKeplerLine2" value="1 88888U 98067A   11291.79166666  .00073094  13844-3  66816-4 0  8" />
     <CT:setting name="ProbKeplerLine3" value="2 88888 072.8435 115.9689 0086731 052.6988 110.5714 16.05824518704292" />


<!-- target point on the Moon -->
    <CT:setting name="Targetlongitude" value="-15" />
    <CT:setting name="Targetlatitude" value="-2" />
    <CT:setting name="SunM" value="1.9884158296478392e+030" />
    <CT:setting name="EarthR" value="6371000" />
    <CT:setting name="EarthRP" value="6356800" />
    <CT:setting name="EarthRE" value="6378100" />
    <CT:setting name="EarthM" value="5.9721863856475894e+024" />
    <CT:setting name="MassRatioSunToEarthPlusMoon" value="328900.56" />
    <CT:setting name="EarthTSolSec" value="86164.098903691003" />
    <CT:setting name="EarthEpoch" value="11036.971719672511" />
    <CT:setting name="EarthAph" value="152097701000" />
    <CT:setting name="EarthPer" value="147098074000" />
    <CT:setting name="EarthSmAx" value="149597887500" />
    <CT:setting name="EarthSmAxAU" value="1.0000001124" />
    <CT:setting name="EarthEcc" value="0.016705878169365421" />
    <CT:setting name="EarthTDays" value="365.25636600000001" />
    <CT:setting name="EarthIncl" value="0" />
    <CT:setting name="EarthAscNode" value="348.73936000000003" />
    <CT:setting name="EarthArgPer" value="114.20783" />
    <CT:setting name="EarthMeanAnom" value="357.51715999999999" />
    <CT:setting name="MoonR" value="1737100" />
    <CT:setting name="MoonRP" value="1735970" />
    <CT:setting name="MoonRE" value="1738140" />
    <CT:setting name="MoonM" value="7.3458114403351352e+022" />

<!--next line will force recalculation of SunM based on G constant -->
    <CT:setting name="GMSun" value="1.327124400350198e+020" />
    <CT:setting name="GMEarthMoon" value="403503241737999.87" />
    <CT:setting name="GMEarth" value="398600441499999.87" />
    <CT:setting name="GMMoon" value="4902800237999.998" />

<!-- next line will force calculation of a Earth and Moon mass -->
<!-- it is not in use - value just for reference and fo trigger -->
    <CT:setting name="MassRatioEarthToMoon" value="81.300567461545441" />
    <CT:setting name="MoonKeplerLine1" value="MOON" />
    <CT:setting name="MoonKeplerLine2" value="1 MOON00 MOON00   11036.9717196725100000000  00000-0  00000-0 0  0000" />
    <CT:setting name="MoonKeplerLine3" value="2 MOON0  23.3228 347.3796 0638000 185.7146 173.5436 0.036600996000000" />

    <CT:setting name="MoonEpoch" value="11036.971719672511" />
    <CT:setting name="MoonAph" value="405696000" />
    <CT:setting name="MoonPer" value="363104000" />
    <CT:setting name="MoonSmAx" value="0" />
    <CT:setting name="MoonEcc" value="0.063799999999999996" />
    <CT:setting name="MoonTDays" value="27.321660864092333" />
    <CT:setting name="MoonIncl" value="23.322800000000001" />
    <CT:setting name="MoonAscNode" value="347.37959999999998" />
    <CT:setting name="MoonArgPer" value="185.71459999999999" />
    <CT:setting name="MoonMeanAnom" value="173.5436" />

<!-- next line (value == "1.0") will force calculation
                         of a Earth kepler position -->
    <CT:setting name="EarthCalcKepler" value="0.0" />

<!-- next line will force assigning velocities and positions 
     based on JPL data -->

    <CT:setting name="UseJPLxyz" value="1.0" />
    <CT:setting name="StartOptim" value="0" />
   <CT:setting name="MaxOptim" value="8" />


</CT:section>

            <!--     now all engines    -->
<CT:section name="Engine" value="0.0" />
    <CT:setting name="EngineNumber" value="0" />
    <CT:setting name="EngineOnSatellite" value="0" />
    <!-- convinent coeff - instead of entry real values just assume scaled version-->

     <CT:setting name="PropCoeff" value="0.05" />

     <CT:setting name="Weight" value="17.157" />
     <CT:setting name="TotalWeight" value="21.996" />

    <!-- iteration per sec from engine's plot -->
    <CT:setting name="DeltaT" value="5" />

     <!-- 2- EARTH 9-MOON for calculation distanses-->
     <CT:setting name="NearBody" value="2" />

     <!-- calculates 
          0 Perigee to a center of NearBody
          1 Apogee to a center of NearBody
          3 taget practice not far then distance earth-moon
          4 target practice to apoint on a moon's surface 
          8 intial period
     <CT:setting name="Calculate" value="8" />

     <!-- AngleType 0 - tangent line to orbit (elipse) oposit velocity
                    1 - two angles set with reference to NearBody centre direction
                    2 - 3 angles set vector fire (constant all fire) 
                    3 - oposit vector of velocity
                    4 - same direction as vector of velocity -->
     <CT:setting name="AngleType" value="0" />

     <!-- 2- EARTH 9-MOON for firing angle -->
     <CT:setting name="AngleOnBody" value="2" />

    <!-- first angle: in a plane over vector from the center of NearBody and Sat
         and vector of velocity. Angle: Centre,Sat,Direction 
         (aggle == 90 degr is a Tangent line to elipse) -->
         <CT:setting name="FireAng1" value="1" />

     <!-- second angle from projection of a velocity vector to a  
         plane perpendicular to direction to centre of nearbody -->
    <CT:setting name="FireAng2" value="1" />

    <CT:setting name="XVector" value="-1" />
    <CT:setting name="YVector" value="1.1537307924011437" />
    <CT:setting name="ZVector" value="0.9986199954416527" />

     <CT:setting name="OptimizationInitialStep" value="10" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />

        <CT:setting name="Period" value="5494.000000" />

    <!-- set impulses in a time -->
        <CT:setting name="FireTime" value="11944" />

     <CT:setting name="ImplVal" value="0.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3000.0" />
     <CT:setting name="ImplVal" value="3100.0" />
     <CT:setting name="ImplVal" value="3500.0" />

     <CT:setting name="ImplVal" value="3550.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3700.0" />
     <CT:setting name="ImplVal" value="3750.0" />

     <CT:setting name="ImplVal" value="3800.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3900.0" />                                      
     <CT:setting name="ImplVal" value="3950.0" />
     <CT:setting name="ImplVal" value="4000.0" />

     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
       
     <CT:setting name="ImplVal" value="3980.0" />
     <CT:setting name="ImplVal" value="3960.0" />
     <CT:setting name="ImplVal" value="3940.0" />
     <CT:setting name="ImplVal" value="3920.0" />
     <CT:setting name="ImplVal" value="3900.0" />

     <CT:setting name="ImplVal" value="3885.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3815.0" />
     <CT:setting name="ImplVal" value="3780.0" />
     <CT:setting name="ImplVal" value="3745.0" />

     <CT:setting name="ImplVal" value="3710.0" />
     <CT:setting name="ImplVal" value="3695.0" />
     <CT:setting name="ImplVal" value="3680.0" />
     <CT:setting name="ImplVal" value="3665.0" />
     <CT:setting name="ImplVal" value="3650.0" />

     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3150.0" />

     <CT:setting name="ImplVal" value="2000.0" />
     <CT:setting name="ImplVal" value="250.0" />
     <CT:setting name="ImplVal" value="0.0" />

</CT:section>


<CT:section name="Engine" value="1" />
    <CT:setting name="EngineNumber" value="1" />
    <CT:setting name="EngineOnSatellite" value="0" />
    <!-- convinent coeff - instead of entry real values just assume scaled version-->
     <CT:setting name="PropCoeff" value="0.05" />

     <CT:setting name="Weight" value="17.157" />
     <CT:setting name="TotalWeight" value="21.996" />


    <!-- iteration per sec from engine's plot -->
    <CT:setting name="DeltaT" value="5" />

     <!-- 2- EARTH 9-MOON for calculation distanses-->
     <CT:setting name="NearBody" value="2" />

     <!-- calculates 
          0 Perigee to a center of NearBody
          1 Apogee to a center of NearBody
          3 taget practice not far then distance earth-moon
          4 target practice to apoint on a moon's surface -->
     <CT:setting name="Calculate" value="0" />

     <!-- AngleType 0 - tangent line to orbit (elipse) oposit velocity
                    1 - two angles set with reference to NearBody centre direction
                    2 - 3 angles set vector fire (constant all fire) 
                    3 - oposit vector of velocity
                    4 - same direction as vector of velocity -->
     <CT:setting name="AngleType" value="0" />

     <!-- 2- EARTH 9-MOON for firing angle -->
     <CT:setting name="AngleOnBody" value="2" />

    <!-- first angle: in a plane over vector from the center of NearBody and Sat
         and vector of velocity. Angle: Centre,Sat,Direction 
         (aggle == 90 degr is a Tangent line to elipse) -->
         <CT:setting name="FireAng1" value="0" />

     <!-- second angle from projection of a velocity vector to a  
         plane perpendicular to direction to centre of nearbody -->
    <CT:setting name="FireAng2" value="0" />

    <CT:setting name="XVector" value="1" />
    <CT:setting name="YVector" value="-1.1714976896575997" />
    <CT:setting name="ZVector" value="-1.019984486712751" />

     <CT:setting name="OptimizationInitialStep" value="100" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />

        <CT:setting name="Period" value="5542.000000" />

    <!-- set impulses in a time -->
        <CT:setting name="FireTime" value="25788" />
        <CT:setting name="FireTime" value="28626" />

     <CT:setting name="ImplVal" value="0.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3000.0" />
     <CT:setting name="ImplVal" value="3100.0" />
     <CT:setting name="ImplVal" value="3500.0" />

     <CT:setting name="ImplVal" value="3550.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3700.0" />
     <CT:setting name="ImplVal" value="3750.0" />

     <CT:setting name="ImplVal" value="3800.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3900.0" />                                      
     <CT:setting name="ImplVal" value="3950.0" />
     <CT:setting name="ImplVal" value="4000.0" />

     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
       
     <CT:setting name="ImplVal" value="3980.0" />
     <CT:setting name="ImplVal" value="3960.0" />
     <CT:setting name="ImplVal" value="3940.0" />
     <CT:setting name="ImplVal" value="3920.0" />
     <CT:setting name="ImplVal" value="3900.0" />

     <CT:setting name="ImplVal" value="3885.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3815.0" />
     <CT:setting name="ImplVal" value="3780.0" />
     <CT:setting name="ImplVal" value="3745.0" />

     <CT:setting name="ImplVal" value="3710.0" />
     <CT:setting name="ImplVal" value="3695.0" />
     <CT:setting name="ImplVal" value="3680.0" />
     <CT:setting name="ImplVal" value="3665.0" />
     <CT:setting name="ImplVal" value="3650.0" />

     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3150.0" />

     <CT:setting name="ImplVal" value="2000.0" />
     <CT:setting name="ImplVal" value="250.0" />
     <CT:setting name="ImplVal" value="0.0" />

</CT:section>


<CT:section name="Engine" value="2" />
    <CT:setting name="EngineNumber" value="2" />
    <CT:setting name="EngineOnSatellite" value="0" />
    <!-- convinent coeff - instead of entry real values just assume scaled version-->

     <CT:setting name="PropCoeff" value="3.0" />

     <CT:setting name="Weight" value="17.157" />
     <CT:setting name="TotalWeight" value="21.996" />


    <!-- iteration per sec from engine's plot -->
    <CT:setting name="DeltaT" value="5" />

     <!-- 2- EARTH 9-MOON for calculation distanses-->
     <CT:setting name="NearBody" value="2" />

     <!-- calculates 
          0 Perigee to a center of NearBody
          1 Apogee to a center of NearBody
          3 taget practice not far then distance earth-moon
          4 target practice to apoint on a moon's surface -->
     <CT:setting name="Calculate" value="1" />

     <!-- AngleType 0 - tangent line to orbit (elipse) oposit velocity
                    1 - two angles set with reference to NearBody centre direction
                    2 - 3 angles set vector fire (constant all fire) 
                    3 - oposit vector of velocity
                    4 - same direction as vector of velocity -->
     <CT:setting name="AngleType" value="0" />

     <!-- 2- EARTH 9-MOON for firing angle -->
     <CT:setting name="AngleOnBody" value="2" />

    <!-- first angle: in a plane over vector from the center of NearBody and Sat
         and vector of velocity. Angle: Centre,Sat,Direction 
         (aggle == 90 degr is a Tangent line to elipse) -->
         <CT:setting name="FireAng1" value="0" />

     <!-- second angle from projection of a velocity vector to a  
         plane perpendicular to direction to centre of nearbody -->
    <CT:setting name="FireAng2" value="0" />

    <CT:setting name="XVector" value="1" />
    <CT:setting name="YVector" value="0.85063762129876674" />
    <CT:setting name="ZVector" value="1.4117704154874764" />

     <CT:setting name="OptimizationInitialStep" value="100" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />

        <CT:setting name="Period" value="5590.000000" />

    <!-- set impulses in a time -->
        <CT:setting name="FireTime" value="39810" />

     <CT:setting name="ImplVal" value="0.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3000.0" />
     <CT:setting name="ImplVal" value="3100.0" />
     <CT:setting name="ImplVal" value="3500.0" />

     <CT:setting name="ImplVal" value="3550.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3700.0" />
     <CT:setting name="ImplVal" value="3750.0" />

     <CT:setting name="ImplVal" value="3800.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3900.0" />                                      
     <CT:setting name="ImplVal" value="3950.0" />
     <CT:setting name="ImplVal" value="4000.0" />

     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
       
     <CT:setting name="ImplVal" value="3980.0" />
     <CT:setting name="ImplVal" value="3960.0" />
     <CT:setting name="ImplVal" value="3940.0" />
     <CT:setting name="ImplVal" value="3920.0" />
     <CT:setting name="ImplVal" value="3900.0" />

     <CT:setting name="ImplVal" value="3885.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3815.0" />
     <CT:setting name="ImplVal" value="3780.0" />
     <CT:setting name="ImplVal" value="3745.0" />

     <CT:setting name="ImplVal" value="3710.0" />
     <CT:setting name="ImplVal" value="3695.0" />
     <CT:setting name="ImplVal" value="3680.0" />
     <CT:setting name="ImplVal" value="3665.0" />
     <CT:setting name="ImplVal" value="3650.0" />

     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3150.0" />

     <CT:setting name="ImplVal" value="2000.0" />
     <CT:setting name="ImplVal" value="250.0" />
     <CT:setting name="ImplVal" value="0.0" />
</CT:section>


<CT:section name="Engine" value="3" />
    <CT:setting name="EngineNumber" value="3" />
    <CT:setting name="EngineOnSatellite" value="0" />
    <!-- convinent coeff - instead of entry real values just assume scaled version-->

     <CT:setting name="PropCoeff" value="0.1" />

     <CT:setting name="Weight" value="17.157" />
     <CT:setting name="TotalWeight" value="21.996" />

    <!-- iteration per sec from engine's plot -->
    <CT:setting name="DeltaT" value="5" />

     <!-- 2- EARTH 9-MOON for calculation distanses-->
     <CT:setting name="NearBody" value="9" />

     <!-- calculates 
          0 Perigee to a center of NearBody
          1 Apogee to a center of NearBody
          3 taget practice not far then distance earth-moon
          4 target practice to apoint on a moon's surface -->
     <CT:setting name="CalculateAP" value="5" />

     <!-- AngleType 0 - tangent line to orbit (elipse) oposit velocity
                    1 - two angles set with reference to NearBody centre direction
                    2 - 3 angles set vector fire (constant all fire) 
                    3 - oposit vector of velocity
                    4 - same direction as vector of velocity -->
     <CT:setting name="AngleType" value="2" />

     <!-- 2- EARTH 9-MOON for firing angle -->
     <CT:setting name="AngleOnBody" value="9" />

    <!-- first angle: in a plane over vector from the center of NearBody and Sat
         and vector of velocity. Angle: Centre,Sat,Direction 
         (aggle == 90 degr is a Tangent line to elipse) -->
         <CT:setting name="FireAng1" value="0" />

     <!-- second angle from projection of a velocity vector to a  
         plane perpendicular to direction to centre of nearbody -->
    <CT:setting name="FireAng2" value="0" />

    <CT:setting name="XVector" value="1.483789" />
    <CT:setting name="YVector" value="-0.097251000000000004" />
    <CT:setting name="ZVector" value="0.56240299999999999" />

     <CT:setting name="OptimizationInitialStep" value="0.25" />
     <CT:setting name="OptimizationDecCoef" value="2" />
     <CT:setting name="OptimizationStop" value="1.0000000000000001e-005" />

    <!-- set impulses in a time -->
        <CT:setting name="FireTime" value="650000" />

     <CT:setting name="ImplVal" value="0.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3000.0" />
     <CT:setting name="ImplVal" value="3100.0" />
     <CT:setting name="ImplVal" value="3500.0" />

     <CT:setting name="ImplVal" value="3550.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3700.0" />
     <CT:setting name="ImplVal" value="3750.0" />

     <CT:setting name="ImplVal" value="3800.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3900.0" />                                      
     <CT:setting name="ImplVal" value="3950.0" />
     <CT:setting name="ImplVal" value="4000.0" />

     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
       
     <CT:setting name="ImplVal" value="3980.0" />
     <CT:setting name="ImplVal" value="3960.0" />
     <CT:setting name="ImplVal" value="3940.0" />
     <CT:setting name="ImplVal" value="3920.0" />
     <CT:setting name="ImplVal" value="3900.0" />

     <CT:setting name="ImplVal" value="3885.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3815.0" />
     <CT:setting name="ImplVal" value="3780.0" />
     <CT:setting name="ImplVal" value="3745.0" />

     <CT:setting name="ImplVal" value="3710.0" />
     <CT:setting name="ImplVal" value="3695.0" />
     <CT:setting name="ImplVal" value="3680.0" />
     <CT:setting name="ImplVal" value="3665.0" />
     <CT:setting name="ImplVal" value="3650.0" />

     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3150.0" />

     <CT:setting name="ImplVal" value="2000.0" />
     <CT:setting name="ImplVal" value="250.0" />
     <CT:setting name="ImplVal" value="0.0" />

</CT:section>


<CT:section name="Engine" value="4" />
    <CT:setting name="EngineNumber" value="4" />
    <CT:setting name="EngineOnSatellite" value="0" />
    <!-- convinent coeff - instead of entry real values just assume scaled version-->

     <CT:setting name="PropCoeff" value="0.25" />

     <CT:setting name="Weight" value="17.157" />
     <CT:setting name="TotalWeight" value="21.996" />


    <!-- iteration per sec from engine's plot -->
    <CT:setting name="DeltaT" value="5" />

     <!-- 2- EARTH 9-MOON for calculation distanses-->
     <CT:setting name="NearBody" value="9" />

     <!-- calculates 
          0 Perigee to a center of NearBody
          1 Apogee to a center of NearBody
          3 taget practice not far then distance earth-moon
          4 target practice to apoint on a moon's surface -->
     <CT:setting name="CalculateAP" value="0" />

     <!-- AngleType 0 - tangent line to orbit (elipse) oposit velocity
                    1 - two angles set with reference to NearBody centre direction
                    2 - 3 angles set vector fire (constant all fire) 
                    3 - oposit vector of velocity
                    4 - same direction as vector of velocity -->
     <CT:setting name="AngleType" value="4" />

     <!-- 2- EARTH 9-MOON for firing angle -->
     <CT:setting name="AngleOnBody" value="9" />

    <!-- first angle: in a plane over vector from the center of NearBody and Sat
         and vector of velocity. Angle: Centre,Sat,Direction 
         (aggle == 90 degr is a Tangent line to elipse) -->
         <CT:setting name="FireAng1" value="0" />

     <!-- second angle from projection of a velocity vector to a  
         plane perpendicular to direction to centre of nearbody -->
    <CT:setting name="FireAng2" value="0" />

    <CT:setting name="XVector" value="-780.76188869660473" />
    <CT:setting name="YVector" value="-2363.0551757693047" />
    <CT:setting name="ZVector" value="-454.32231393279926" />

     <CT:setting name="OptimizationInitialStep" value="0.10000000000000001" />
     <CT:setting name="OptimizationDecCoef" value="2" />
     <CT:setting name="OptimizationStop" value="0.10000000000000001" />

    <!-- set impulses in a time -->
        <CT:setting name="FireTime" value="772052" />

     <CT:setting name="ImplVal" value="0.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3000.0" />
     <CT:setting name="ImplVal" value="3100.0" />
     <CT:setting name="ImplVal" value="3500.0" />

     <CT:setting name="ImplVal" value="3550.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3700.0" />
     <CT:setting name="ImplVal" value="3750.0" />

     <CT:setting name="ImplVal" value="3800.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3900.0" />                                      
     <CT:setting name="ImplVal" value="3950.0" />
     <CT:setting name="ImplVal" value="4000.0" />

     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
     <CT:setting name="ImplVal" value="4000.0" />
       
     <CT:setting name="ImplVal" value="3980.0" />
     <CT:setting name="ImplVal" value="3960.0" />
     <CT:setting name="ImplVal" value="3940.0" />
     <CT:setting name="ImplVal" value="3920.0" />
     <CT:setting name="ImplVal" value="3900.0" />

     <CT:setting name="ImplVal" value="3885.0" />
     <CT:setting name="ImplVal" value="3850.0" />
     <CT:setting name="ImplVal" value="3815.0" />
     <CT:setting name="ImplVal" value="3780.0" />
     <CT:setting name="ImplVal" value="3745.0" />

     <CT:setting name="ImplVal" value="3710.0" />
     <CT:setting name="ImplVal" value="3695.0" />
     <CT:setting name="ImplVal" value="3680.0" />
     <CT:setting name="ImplVal" value="3665.0" />
     <CT:setting name="ImplVal" value="3650.0" />

     <CT:setting name="ImplVal" value="3600.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3500.0" />
     <CT:setting name="ImplVal" value="3400.0" />
     <CT:setting name="ImplVal" value="3150.0" />

     <CT:setting name="ImplVal" value="2000.0" />
     <CT:setting name="ImplVal" value="250.0" />
     <CT:setting name="ImplVal" value="0.0" />

</CT:section>
<CT:section name="Optim" value="0" />
<!-- do optimization of an engine N... (0,1,2,3...)
     it is posible to use 4 engines but optimize engine 3-->

    <CT:setting name="EngineToOptimize" value="0" />

<!-- Type of optimization
      1 - search for a minimum by adjusting time of firing
      2 - search for a maximum by adjusting time of firing
      3 - search for minimum by adjusting time of firing
      4 - search fo minimum by adjusting angle of firing
  initial step and decrease steps for each search specified
  individualy for each engine -->

    <CT:setting name="TrajectoryOptimizationType" value="2" />
     <!-- 2- EARTH 9-MOON for calculation distanses-->
     <CT:setting name="NearBody" value="2" />

     <!-- calculates 
          0 Perigee to a center of NearBody
          1 Apogee to a center of NearBody
          3 taget practice not far then distance earth-moon
          4 target practice to a point on a moon's surface 
          8 intial period
     <CT:setting name="Calculate" value="8" />

<!-- last used engine (0,1,2,3..) in trajectory optimization or calculations 
     setting lastengine == -1 disable optimization -->

    <CT:setting name="LastEngine" value="-1" />

</CT:section>

<CT:section name="Optim" value="1" />
        <CT:setting name="EngineToOptimize" value="0" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="9" />
     <CT:setting name="OptimizationInitialStep" value="10" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="0" />
</CT:section>

<CT:section name="Optim" value="2" />
        <CT:setting name="EngineToOptimize" value="0" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="1" />
        <CT:setting name="OptimizationInitialStep" value="10" />
        <CT:setting name="OptimizationDecCoef" value="10" />
        <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="0" />
</CT:section>

<CT:section name="Optim" value="3" />
        <CT:setting name="EngineToOptimize" value="1" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="8" />
     <CT:setting name="OptimizationInitialStep" value="10" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="1" />
</CT:section>

<CT:section name="Optim" value="4" />
        <CT:setting name="EngineToOptimize" value="1" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="10" />
     <CT:setting name="OptimizationInitialStep" value="100" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="1" />
</CT:section>

<CT:section name="Optim" value="5" />
        <CT:setting name="EngineToOptimize" value="1" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="0" />
     <CT:setting name="OptimizationInitialStep" value="100" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="1" />
</CT:section>

<CT:section name="Optim" value="6" />
        <CT:setting name="EngineToOptimize" value="2" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="8" />
     <CT:setting name="OptimizationInitialStep" value="100" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="2" />
</CT:section>

<CT:section name="Optim" value="7" />
        <CT:setting name="EngineToOptimize" value="2" />
        <CT:setting name="TrajectoryOptimizationType" value="2" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="11" />
     <CT:setting name="OptimizationInitialStep" value="0.01" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="0.0001" />
        <CT:setting name="LastEngine" value="2" />
</CT:section>


<CT:section name="Optim" value="8" />
        <CT:setting name="EngineToOptimize" value="2" />
        <CT:setting name="TrajectoryOptimizationType" value="6" />
        <CT:setting name="NearBody" value="2" />
        <CT:setting name="Calculate" value="12" />
     <CT:setting name="OptimizationInitialStep" value="0.01" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="0.0001" />
        <CT:setting name="LastEngine" value="2" />
</CT:section>

<CT:section name="Optim" value="9" />
        <CT:setting name="EngineToOptimize" value="2" />
        <CT:setting name="TrajectoryOptimizationType" value="1" />
        <CT:setting name="NearBody" value="9" />
        <CT:setting name="Calculate" value="0" />
     <CT:setting name="OptimizationInitialStep" value="100" />
     <CT:setting name="OptimizationDecCoef" value="10" />
     <CT:setting name="OptimizationStop" value="1" />
        <CT:setting name="LastEngine" value="2" />
</CT:section>

<CT:section name="Optim" value="10" />
<!-- calculates perigee to the Moon, search for minimum by adjusting time -->
           <CT:setting name="EngineToOptimize" value="2" />
           <CT:setting name="TrajectoryOptimizationType" value="6" />
           <CT:setting name="NearBody" value="9" />
           <CT:setting name="Calculate" value="0" />
           <CT:setting name="OptimizationInitialStep" value="0.01" />
           <CT:setting name="OptimizationDecCoef" value="10" />
           <CT:setting name="OptimizationStop" value="0.0001" />
           <CT:setting name="LastEngine" value="2" />

        <CT:setting name="Period" value="5358.000000" />
</CT:section>

<CT:section name="Optim" value="10" />
<!-- calculates perigee to the Moon, search for minimum by adjusting time -->
           <CT:setting name="EngineToOptimize" value="2" />
           <CT:setting name="TrajectoryOptimizationType" value="6" />
           <CT:setting name="NearBody" value="9" />
           <CT:setting name="Calculate" value="0" />
           <CT:setting name="OptimizationInitialStep" value="0.01" />
           <CT:setting name="OptimizationDecCoef" value="10" />
           <CT:setting name="OptimizationStop" value="0.0001" />
           <CT:setting name="LastEngine" value="2" />

        <CT:setting name="Period" value="5358.000000" />
</CT:section>


</CT:data>
