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ball_orbit.xml
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ball_orbit.xml
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<?xml version="1.0" encoding="UTF-8"?>
<?xml-stylesheet type="text/xsl" href="http://jsbsim.sf.net/JSBSimScript.xsl"?>
<runscript xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:noNamespaceSchemaLocation="http://jsbsim.sf.net/JSBSimScript.xsd"
name="cannon ball test">
<use aircraft="ball" initialize="reset00_v2"/>
<run start="0.0" end="10800" dt="0.005">
<description>
Integrators
0: No integrator (Freeze)
1: Rectangular Euler
2: Trapezoidal
3: Adams Bashforth 2
4: Adams Bashforth 3
5: Adams Bashforth 4
</description>
<property value="3"> simulation/integrator/rate/rotational </property>
<property value="3"> simulation/integrator/rate/translational </property>
<property value="1"> simulation/integrator/position/rotational </property>
<property value="4"> simulation/integrator/position/translational </property>
<property value="1"> simulation/gravity-model </property>
<property value="0"> simulation/output[0]/log_rate_hz </property>
<property> simulation/notify-time-trigger </property>
<!--property value="25000"> ic/u-fps </property>
<property value="-7000"> ic/v-fps </property-->
<event name="Time Notify" persistent="true">
<description>Output message at 10 minute intervals</description>
<notify>
<property caption="Height AGL (ft): "> position/h-agl-ft </property>
<property caption="Altitude (Geod, ft): "> position/geod-alt-ft </property>
<property caption="Latitude (Geod, deg): "> position/lat-geod-deg </property>
<property caption="Vehicle Radius (ft): "> position/radius-to-vehicle-ft </property>
<property caption="Inertial Vel Mag (ft/s): "> velocities/eci-velocity-mag-fps </property>
<property caption="Body X Velocity (ft/s): "> velocities/u-fps </property>
<property caption="Simulation Frame: "> simulation/frame </property>
<property caption="Density: "> atmosphere/rho-slugs_ft3 </property>
<property caption="Angular momentum (ft^2/s)"> orbital/specific-angular-momentum-ft2_sec </property>
<property caption="Inclination (deg) "> orbital/inclination-deg </property>
<property caption="Right ascension (deg) "> orbital/right-ascension-deg </property>
<property caption="Argument of perigee (deg)"> orbital/argument-of-perigee-deg </property>
<property caption="Period (s) "> orbital/period-sec </property>
<property caption="Eccentricity "> orbital/eccentricity </property>
<property caption="Apoapsis radius (ft) "> orbital/apoapsis-radius-ft </property>
<property caption="Periapsis radius (ft) "> orbital/periapsis-radius-ft </property>
<property caption="True anomaly (deg) "> orbital/true-anomaly-deg </property>
</notify>
<condition> simulation/sim-time-sec >= simulation/notify-time-trigger </condition>
<set name="simulation/notify-time-trigger" value="600" type="FG_DELTA"/>
</event>
<!--event name="Final Data Point">
<description> Log data on command </description>
<notify>
<property caption="Simulation Time: "> simulation/sim-time-sec </property>
<property caption="Height AGL (ft): "> position/h-agl-ft </property>
<property caption="Altitude (Geod, ft): "> position/geod-alt-ft </property>
<property caption="Latitude (Geod, deg): "> position/lat-geod-deg </property>
<property caption="Vehicle Radius (ft): "> position/radius-to-vehicle-ft </property>
<property caption="Inertial Vel Mag (ft/s): "> velocities/eci-velocity-mag-fps </property>
<property caption="Body X Velocity (ft/s): "> velocities/u-fps </property>
<property caption="Simulation Frame: "> simulation/frame </property>
</notify>
<condition> simulation/sim-time-sec >= 86400.0 </condition>
<set name="simulation/force-output" value="0"/>
</event-->
</run>
</runscript>