<?xml version="1.0" encoding="iso-8859-1" ?>
<CRRCSim_airplane version="2">
  <name>
    <en>Flexifly XLM</en>
  </name>
  <categories>
    <category>Powered gliders</category>
    <category>Electric</category>
    <category>Foamies</category>
  </categories>
  <description>
    <en>The Pemotec FlexiflyXLM (http://www.pemotec.com). A 1 m glider made of EPP.</en>
  </description>
  <changelog>
    <change>
      <date>2006-01-01</date>
      <author>Jan Reucker (slowhand_47@gmx.de)</author>
      <en>Calculated FDM parameters using AVL</en>
    </change>
    <change>
      <date>2006-01-08</date>
      <author>CRRCSim 0.9.5</author>
      <en>Automatically converted from .air file.</en>
    </change>
    <change>
      <date>2006-02-18</date>
      <author>Jan Reucker (slowhand_47@gmx.de)</author>
      <en>Corrected location of the hardpoints.</en>
    </change>
    <change>
      <date>2006-12-31</date>
      <author>Jan Reucker (slowhand_47@gmx.de)</author>
      <en>Added brushless configuration and animations.</en>
    </change>
    <change>
      <date>2006-01-28</date>
      <author>Jan Reucker (slowhand_47@gmx.de)</author>
      <en>New aero and mass parameters calculated by Jens W. Wulf.
      Removed brushless configuration (does not work with the new
      set of parameters). Reduced spring damping of the hardpoints
      to avoid the black screen phenomenon when landing inverted.</en>
    </change>
    <change>
      <date>2006-04-01</date>
      <author>Jan Reucker (slowhand_47@gmx.de)</author>
      <en>Adapted animations to file format changes.</en>
    </change>
    <change>
      <date>2009-02-25</date>
      <author>Jens W. Wulf</author>
      <en>Added launch default</en>
    </change>
    <change>
      <date>2010-05-13</date>
      <author>J. Reucker</author>
      <en>Added max_force to springs</en>
    </change>
  </changelog>
  <aero version="1" units="1">
    <ref chord="0.14960092" span="1.00076" area="0.14814809" speed="19" />
    <l Cl_b="-0.135825" Cl_p="-0.484121" Cl_r="0.166927" Cl_da="-0.009558" Cl_dr="0" />
    <m Cm_a="-0.587625" Cm_q="-9.86444" Cm_0="0" Cm_de="-0.554186" />
    <n Cn_b="0.073321" Cn_p="-0.043168" Cn_r="-0.076957" Cn_da="0.041483" Cn_dr="0" />
    <Y CY_b="-0.25642" CY_p="-0.084046" CY_r="0.231354" CY_da="-0.101438" CY_dr="0" />
    <lift CL_a="4.927615" CL_q="6.933846" CL_0="0.6" CL_de="0.23446" CL_max="1.1"
       CL_min="-0.6" CL_drop="0.5" CL_CD0="0.2" />
    <misc Alpha_0="0.055962412" span_eff="0.95" eta_loc="0.15" CG_arm="0.25" />
    <drag CD_prof="0.02" Uexp_CD="-0.5" CD_stall="0" CD_CLsq="0.013" CD_AIsq="0"
       CD_ELsq="0" />
  </aero>

  <config version="1">
    <descr_long>
      <en>Default configuration with a Speed 400 brushed motor on 7 NiMH cells.</en>
    </descr_long>
    <descr_short>
      <en>Speed 400</en>
    </descr_short>
    <mass_inertia version="1" units="1" Mass="0.4305" I_xx="0.0046434488"
       I_yy="0.0057315134" I_zz="0.0097620834" I_xz="0.00012791619" />
    <sound version="1">
      <sample filename="electric.wav" type="1" pitchfactor="0.004" maxvolume="1.0" />
    </sound>
    
    <power units="1">
        <battery filename="nimh7_kan1050" throttle_min="0">
          <shaft J="0" brake="1">
            <propeller D="0.15" H="0.075" J="0" n_fold="5" >
              <pos x="0.09" downthrust="6" />
            </propeller>
            <engine filename="Mabuchi_380_FR" />
          </shaft>
        </battery>
    </power>
  </config>
  <graphics version="1" model="flexifly_xlm.ac">
    <descr_long>
      <en>Automatically converted from FlexiflyXLM.air.</en>
    </descr_long>
    <descr_short>
      <en>default</en>
    </descr_short>
  </graphics>
  <wheels version="1" units="0">
  
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- right wingtip -->
      <pos x="0.14" y="1.65" z="-0.21" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- right wingtip -->
      <pos x="-0.28" y="1.65" z="-0.21" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- left wingtip -->
      <pos x="0.14" y="-1.65" z="-0.21" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- left wingtip -->
      <pos x="-0.28" y="-1.65" z="-0.21" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- right inner wing -->
      <pos x="0.14" y="0.8" z="-0.05" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- left inner wing -->
      <pos x="0.14" y="-0.8" z="-0.05" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- right horiz stab -->
      <pos x="-1.32" y="0.57" z="0.0" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- right horiz stab -->
      <pos x="-1.53" y="0.57" z="0.0" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- left horiz stab -->
      <pos x="-1.32" y="-0.57" z="0.0" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- left horiz stab -->
      <pos x="-1.53" y="-0.57" z="0.0" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- vert stab -->
      <pos x="-1.58" y="0.0" z="-0.48" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- vert stab -->
      <pos x="-1.34" y="0.0" z="-0.48" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- nose -->
      <pos x="0.67" y="0.0" z="0.11" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- fuselage front -->
      <pos x="0.25" y="0.0" z="0.25" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
    <wheel percent_brake="1.0" caster_angle_rad="0.0"> <!-- fuselage rear -->
      <pos x="-1.56" y="0.0" z="0.05" />
      <spring constant="10.0" damping="0.05" max_force="4.5" />
    </wheel>
  </wheels>
  <animations>
    <animation type="ControlSurface">
      <!-- elevator -->
      <object name="hfin" max_angle="0.35" />
      <control mapping="ELEVATOR" gain="1.0" />
      <hinge x="-1.40" y="0.00" z="-0.01" />
      <hinge x="-1.40" y="1.00" z="-0.01" />
    </animation>
    <animation type="ControlSurface">
      <!-- rudder (controlled by AILERON) -->
      <object name="vfin" max_angle="0.500" />
      <control mapping="AILERON" gain="-1.0" />
      <hinge x="-1.42" y="0.00" z="-0.48" />
      <hinge x="-1.42" y="0.00" z="0.06" />
    </animation>
  </animations>
  <launch>
    <preset name_en="glider default (hand)" altitude="6" velocity_rel="1" angle="0" sal="0" rel_to_player="1" rel_front="0" rel_right="2" />
  </launch>  
</CRRCSim_airplane>
