From: Jon S. B. <jb...@us...> - 2004-04-24 17:13:15
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Update of /cvsroot/jsbsim/JSBSim/scripts In directory sc8-pr-cvs1.sourceforge.net:/tmp/cvs-serv9733/scripts Modified Files: B747-1.xml Log Message: Changes to the Propagate mode - removed VRP items to FGAuxiliary, etc.; removed FGTurbine Index: B747-1.xml =================================================================== RCS file: /cvsroot/jsbsim/JSBSim/scripts/B747-1.xml,v retrieving revision 1.2 retrieving revision 1.3 diff -C2 -r1.2 -r1.3 *** B747-1.xml 12 Nov 2003 03:25:45 -0000 1.2 --- B747-1.xml 24 Apr 2004 17:13:00 -0000 1.3 *************** *** 1,55 **** ! <?xml version="1.0"?> ! <runscript name="B747-400 takeoff run"> ! <!-- ! This run is for testing B747-400 runs ! --> ! ! <use aircraft="B747"> ! <use initialize="reset00"> ! <run start="0.0" end="140" dt="0.00833333"> ! <when> ! <parameter name="sim-time-sec" comparison="ge" value="0.25"> ! <parameter name="sim-time-sec" comparison="le" value="1.00"> ! <set name="propulsion/active_engine" type="FG_VALUE" value="-1" action="FG_STEP" persistent="false"> ! <set name="fcs/throttle-cmd-norm[0]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="fcs/throttle-cmd-norm[1]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="fcs/throttle-cmd-norm[2]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="fcs/throttle-cmd-norm[3]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="propulsion/starter_cmd" type="FG_VALUE" value="1" action="FG_STEP" persistent="false" tc ="1.00"> ! </when> ! ! <when> ! <parameter name="propulsion/n2" comparison="ge" value="15"> ! <set name="fcs/throttle-cmd-norm[0]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="fcs/throttle-cmd-norm[1]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="fcs/throttle-cmd-norm[2]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="fcs/throttle-cmd-norm[3]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="propulsion/cutoff_cmd" type="FG_VALUE" value="0" action="FG_STEP" persistent="false" tc ="1.00"> ! </when> ! ! <when> <!-- Set the Elevator to takeoff --> ! <parameter name="aero/qbar-psf" comparison="ge" value="17.0"> ! <parameter name="position/h-sl-ft" comparison="le" value="2000"> ! <set name="fcs/elevator-cmd-norm" type="FG_VALUE" value="-0.5" action="FG_RAMP" persistent="false" tc ="2.0"> ! </when> ! <!-- ! <when> ! <parameter name="position/h-sl-ft" comparison="ge" value="2000"> ! <parameter name="attitude/theta-rad" comparison="ge" value="0.30"> ! <set name="fcs/elevator-cmd-norm" type="FG_DELTA" value="0.06" action="FG_EXP" persistent="true" tc ="12.0"> ! </when> ! ! <when> ! <parameter name="position/h-sl-ft" comparison="le" value="2000"> ! <parameter name="attitude/theta-rad" comparison="le" value="0.25"> ! <set name="fcs/elevator-cmd-norm" type="FG_DELTA" value="-0.06" action="FG_EXP" persistent="true" tc ="12.0"> ! </when> ! ! <when> ! <parameter name="position/h-sl-ft" comparison="ge" value="2000"> ! <set name="fcs/elevator-cmd-norm" type="FG_VALUE" value="0.00" action="FG_EXP" persistent="false" tc ="1.0"> ! </when> ! --> ! </run> ! ! </runscript> --- 1,55 ---- ! <?xml version="1.0"?> ! <runscript name="B747-400 takeoff run"> ! <!-- ! This run is for testing B747-400 runs ! --> ! ! <use aircraft="B747"> ! <use initialize="reset00"> ! <run start="0.0" end="140" dt="0.00833333"> ! <when> ! <parameter name="sim-time-sec" comparison="ge" value="0.25"> ! <parameter name="sim-time-sec" comparison="le" value="1.00"> ! <set name="propulsion/active_engine" type="FG_VALUE" value="-1" action="FG_STEP" persistent="false"> ! <set name="fcs/throttle-cmd-norm[0]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="fcs/throttle-cmd-norm[1]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="fcs/throttle-cmd-norm[2]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="fcs/throttle-cmd-norm[3]" type="FG_VALUE" value="0.3" action="FG_RAMP" persistent="false" tc ="2.0"> ! <set name="propulsion/starter_cmd" type="FG_VALUE" value="1" action="FG_STEP" persistent="false" tc ="1.00"> ! </when> ! ! <when> ! <parameter name="propulsion/n2" comparison="ge" value="15"> ! <set name="fcs/throttle-cmd-norm[0]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="fcs/throttle-cmd-norm[1]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="fcs/throttle-cmd-norm[2]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="fcs/throttle-cmd-norm[3]" type="FG_VALUE" value="1.0" action="FG_RAMP" persistent="false" tc ="0.05"> ! <set name="propulsion/cutoff_cmd" type="FG_VALUE" value="0" action="FG_STEP" persistent="false" tc ="1.00"> ! </when> ! ! <when> <!-- Set the Elevator to takeoff --> ! <parameter name="aero/qbar-psf" comparison="ge" value="17.0"> ! <parameter name="position/h-sl-ft" comparison="le" value="2000"> ! <set name="fcs/elevator-cmd-norm" type="FG_VALUE" value="-0.5" action="FG_RAMP" persistent="false" tc ="2.0"> ! </when> ! <!-- ! <when> ! <parameter name="position/h-sl-ft" comparison="ge" value="2000"> ! <parameter name="attitude/theta-rad" comparison="ge" value="0.30"> ! <set name="fcs/elevator-cmd-norm" type="FG_DELTA" value="0.06" action="FG_EXP" persistent="true" tc ="12.0"> ! </when> ! ! <when> ! <parameter name="position/h-sl-ft" comparison="le" value="2000"> ! <parameter name="attitude/theta-rad" comparison="le" value="0.25"> ! <set name="fcs/elevator-cmd-norm" type="FG_DELTA" value="-0.06" action="FG_EXP" persistent="true" tc ="12.0"> ! </when> ! ! <when> ! <parameter name="position/h-sl-ft" comparison="ge" value="2000"> ! <set name="fcs/elevator-cmd-norm" type="FG_VALUE" value="0.00" action="FG_EXP" persistent="false" tc ="1.0"> ! </when> ! --> ! </run> ! ! </runscript> |