Mako/mako-yasim.xml

<?xml version="1.0" encoding="ISO-8859-1"?>
<!--  MAKO
	sources:
	http://www.airforce-technology.com/projects/mako/
	https://www.forecastinternational.com/archive/disp_pdf.cfm?DACH_RECNO=840
 -->

<airplane mass="9886" version="YASIM_VERSION_CURRENT">

  <!-- Approach configuration -->
  <approach speed="120" aoa="5" fuel="0.2">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.2"/>
    <control-setting axis="/controls/flight/flaps" value="0.75"/>
    <control-setting axis="/controls/gear/gear-down" value="1"/>
    <control-setting axis="/velocities/airspeed-kt" value="120"/> 
    <control-setting axis="/orientation/alpha-deg" value="5.0"/> 
  </approach>

  <!-- Cruise configuration.   -->
  <cruise speed="860" alt="40000" fuel="0.8">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
    <control-setting axis="/controls/flight/flaps" value="0.0"/>
    <control-setting axis="/controls/gear/gear-down" value="0"/>
    <!--control-setting axis="/controls/flight/elevator-trim" value="-0.1"/-->
  </cruise>

  <!-- pilot eyepoint -->
  <cockpit x="4.0" y="0.0" z=".80"/>

 <!-- <fuselage ax="3.75" ay="0" az="-0.136" bx="-4.5" by="0" bz="-0.0" width="1.5" midpoint= "0" taper="0.7" idrag="0.1"/>-->
  <fuselage ax="7.5" ay="0" az="-0.2" bx="4.8" by="0" bz="0.1" width="1.1" midpoint= "1" taper="0.1" />
  <fuselage ax="-4.4" ay="0" az="0" bx="-5.5" by="0" bz="0" cx="0.01" width="1.0" midpoint= "0" taper="0.5" />
  
  <fuselage ax="5" ay="0" az="0.1" bx="-4.4" by="0" bz="0.0" cx="0.1" width="1.4" midpoint= ".2" taper="0.7" />
  <fuselage ax="6" ay="0" az="0.3" bx="4" by="0" bz="0.9" cx="0.6" width="0.8" midpoint= "1" taper="0.0" />
  <fuselage ax="-1" ay="0" az="0.4" bx="4.2" by="0" bz="0.9" cx="0.01" width="0.8" midpoint= "1" taper="0.0" />

     <!--  
  <fuselage ax="2.5" ay="-0.5" az="-0.636" bx="-4.5" by="0" bz="-0.45" width="1.1" midpoint= "1" taper="0.6" idrag="0.7" />
  <fuselage ax="2.5" ay="0.5" az="-0.636" bx="-4.5" by="0" bz="-0.45" width="1.1" midpoint= "1" taper="0.6" idrag="0.7"/>
-->
  
  
  
  <mstab x="1.1" y="0.60" z="0.3"
         chord="3.7"
         length="1.1"
         taper="1" 
         sweep="42"
         camber="0.01"
         dihedral="0">
         <stall aoa="22" width="13" peak="1.5"/>
         <spoiler start="0.01" end="0.15" lift="-1.05" drag="55.8"/>

         <control-input axis="/controls/flight/speedbrake" control="SPOILER"/>

         <control-output control="SPOILER" prop="/surface-positions/speedbrake-pos-norm"/>

         <control-speed control="SPOILER" transition-time="5.0"/>
  </mstab>
  

  
   <hstab x="-4.3" y="1.05" z="0.15"
         chord="2.4"
         length="1.55"
         taper="0.35" 
         sweep="25"
         dihedral="-4">
         <stall aoa="35" width="23" peak="1.9"/>
	 <flap0 start="0.0" end="1.0" lift="1.8" drag="1.3" />

         <control-input axis="/controls/flight/fcm-elevator" control="FLAP0"/>
	 <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
 	 <control-input axis="/controls/flight/fcm-aileron" control="FLAP0" split="true" src0="-1.0" dst0="-0.6" src1="1.0" dst1="0.6"/>
	 <control-input axis="/controls/flight/aileron-trim" control="FLAP0" split="true" src0="-1.0" dst0="-0.6" src1="1.0" dst1="0.6"/>
	
	 <control-output control="FLAP0" side="left" prop="/surface-positions/left-taileron-pos-norm"/>
	 <control-output control="FLAP0" side="right" prop="/surface-positions/right-taileron-pos-norm"/>
	 <control-output control="FLAP0" prop="/surface-positions/taileron-pos-norm"/>
	 <control-output control="FLAP0" side="left" prop="surface-positions/left-elevator-pos-norm"/>
	 <control-output control="FLAP0" side="right" prop="surface-positions/right-elevator-pos-norm"/>

	 <control-speed control="FLAP0" transition-time="0.5"/>
   </hstab>
  

  <wing x="-0.7" y="1.1" z="0.3"
        chord="4.4"
        length="3.3"
        taper="0.2"
        sweep="24"
	incidence="0.4"
        twist="-0.0"
        camber="0.01"
	dihedral="0.0">
        <stall aoa="21" width="8" peak="1.3"/>
        <flap0 start="0.0" end="0.8" lift="1.2" drag="1.4"/>
		
        <slat start="0.2" end="0.9" lift="1.5" aoa="6" drag="1.1"/>
    
	<!-- Slats are automatically deployed by AoA>7.5 -->
        <control-input axis ="/orientation/alpha-deg" control="SLAT" square="false" src0="7.5" src1="12" dst0="0.0" dst1="1.0"/>
       	<control-input axis="/velocities/airspeed-kt" control="FLAP0" square="false" src0="120" src1="250" dst0="1.0" dst1="0.0"/>
		     
        <control-output control="SLAT" prop="/surface-positions/slat-pos-norm"/>
        <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
        <control-speed control="SLAT" transition-time="1.1"/>
        <control-speed control="FLAP0" transition-time="1"/>
  </wing>

  <vstab x="-3.7" y="0.0" z="0.7"
         chord="3.4"
         length="2.3"
         taper="0.25"
         sweep="23">
         <stall aoa="17" width="6" peak="1.1"/>
         <flap0 start="0.2" end=".9" lift="1.3" drag="1.3"/>

         <control-input axis="/controls/flight/fcm-rudder" control="FLAP0" invert="true"/>
         <control-input axis="/controls/flight/rudder-trim" control="FLAP0" invert="true"/>

         <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>

         <control-speed control="FLAP0" transition-time="1"/>
  </vstab>
 
  

  
  <!--  GE F414M  -->
  
  <jet x="-1.558" y="0.0" z="0"
       mass="2282"  
       thrust="12500"
       afterburner="16850"
       epr="32.1"
       egt="1050"
       n1-idle="25" 
       n1-max="105" 
       n2-idle="30" 
       n2-max="230"
       exhaust-speed="1800"
       tsfc="0.75"
       atsfc="1.85"
       rotation="0">
       <actionpt x="-5.036" y="0.0" z="-0"/>
       <control-input axis="/controls/engines/engine[0]/throttle" src0="0.0" dst0="0.0" src1="0.7" dst1="1.0" control="THROTTLE"/>
       <control-input axis="/controls/engines/engine[0]/throttle" src0="0.72" dst0="0.0" src1="1.0" dst1="1.0" control="REHEAT"/>
       <control-output control="REHEAT" prop="engines/engine[0]/afterburner" />
       <control-speed control="THROTTLE" transition-time="3.1"/>
       <control-speed control="REHEAT" transition-time="5.1"/>
  </jet>

  <!-- gear -->
  <!-- nose -->
  <gear x="4.05" y="0.000" z="-1.75"
        retract-time="7"
        compression="0.7"
        spring="1.1"
	stiction="1"
        damp="1.4">
        <control-input axis="/controls/flight/fcm-rudder" control="STEER" square="false"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
        <control-speed control="EXTEND" transition-time="7"/>
        <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
  </gear>

  <!-- left main -->
  <gear x="-0.9" y="1.434" z="-1.65"
        retract-time="7"
        compression="0.6"
        spring="0.95"
	stiction="1"
	stiction-abs="1"
        damp="2">
        <control-input axis="/controls/gear/brake-left" control="BRAKE"/>
        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
        <control-speed control="EXTEND" transition-time="7"/>
        <control-output control="EXTEND" prop="gear/gear[1]/position-norm"/>
  </gear>

  <!-- right main -->
  <gear x="-0.9" y="-1.434" z="-1.65"
        retract-time="7"
        compression="0.6"
        spring="0.95"
	stiction="1"
	stiction-abs="1"
        damp="2">
        <control-input axis="/controls/gear/brake-right" control="BRAKE"/>
        <control-input axis="/controls/gear/brake-parking" control="BRAKE"/>
        <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
        <control-speed control="EXTEND" transition-time="7"/>
        <control-output control="EXTEND" prop="gear/gear[2]/position-norm"/>
  </gear>

   
  
  
  <!-- Intenal Fuselage tanks -->
  <tank x="4" y="0" z="0" jet="true" capacity="1536"/>

  <tank x="-1" y="0" z="0" jet="true" capacity="1535"/>

  <!-- left wing tanks -->
  <tank x="0" y="2" z="0" jet="true" capacity="1068"/>
  <!-- right wing tanks -->
  <tank x="0" y="-2" z="0" jet="true" capacity="1068"/>
  
  <!-- Drop Tanks - 330 Gal each  -->
  
  <tank x="-0.5" y="2" z="-0.4" jet="true" capacity="2244"/>

  <tank x="0" y="0" z="-1.2" jet="true" capacity="2244"/>
  
  <tank x="-0.5" y="-2" z="-0.4" jet="true" capacity="2244"/>

  <!-- Engine Feed Tank -->

  <tank x="-1.0" y="0.0" z="-0.3" jet="true" capacity="107.5"/>



  
  <!-- CG Theorique x=-2.088 y=0.0 z=-0.551 -->
  <ballast x="3.05" y="0.000" z="-0.5" mass="2500" />
  <!--ballast x="-0.5" y="1.134" z="-1.8" mass="300" /-->
  <!--ballast x="-0.5" y="-1.134" z="-1.8" mass="300" /-->
    

  <!-- external loads -->
  <!-- left  -->  
  <weight x="-1.5" y="4.3" z="0.3" size="0.25" mass-prop="sim/weight[0]/weight-lb"	/>
  <weight x="-1.2" y="3" z="-0.4" size="0.5" mass-prop="sim/weight[1]/weight-lb"/>
  <weight x="-0.5" y="2" z="-0.4" size="0.7" mass-prop="sim/weight[2]/weight-lb"/>


  <!-- Centre -->
  <weight  x="0" y="0" z="-1.2" size="0.7" mass-prop="sim/weight[3]/weight-lb"	/>

  <!--right -->

  <weight x="-0.5" y="-2" z="-0.4"  size="0.7" mass-prop="sim/weight[4]/weight-lb"/>
  <weight x="-1.2" y="-3" z="-0.4" size="0.5" mass-prop="sim/weight[5]/weight-lb"/>
  <weight x="-1.5" y="-4.3" z="0.3" size="0.25" mass-prop="sim/weight[6]/weight-lb"/>  
 
  
</airplane>