CanberraBI8/CanberraBI8-yasim.xml

<!--
    English Electric Canberra B(I)8 yasim config.  This is a hack and
    not an authentic representation of the aircraft.  Having said
    that, the numbers, where I could find them, roughly match those
    of the original aircraft.  Lee Elliott.
-->

<!--
    I found a figure of 21700 lb for the empty a/c but I believe this
    does not include the weight of the crew or non-fuel fluids.
    The max weapon load was 8000 lb and I found a fuel capacity of
    10351 lt internal (2734 US Gal) + 2 x 1109 lt (2 x 293 US Gal) in
    the tips tanks.  Converting these figures into lbs using the 1:6
    ratio that FG seems to use gives 16404 lb internally + 2 x 1758 lb
    in the tip tanks (Tot 19920 lb).
    I also found MTOW of between 48000 lb and 55000 lb, although these
    covered several varients.
    Doing some sums:
    
    Empty weight:       21700
    Tot bomb load:       8000
    Tot fuel load:      19920
                        49620
                        
    As a guesstimate, I've added 1000lb to the empty weight to allow
    for the crew and non-fuel fluids.
    
    I also found a reference to 70-80 kt landing speeds whenthe tanks
    were nearly empty - I've gone for 80 kt with 0.1 (10%) fuel.
-->
<airplane mass="22700" version="YASIM_VERSION_CURRENT">

<!-- Approach configuration -->
  <approach speed="80" aoa="5.0" fuel="0.05">
    <control-setting axis="/controls/engines/engine[0]/throttle" value="0.3"/>
    <control-setting axis="/controls/engines/engine[1]/throttle" value="0.3"/>
    <control-setting axis="/controls/flight/flaps" value="1.0"/>
    <control-setting axis="/controls/flight/spoilers" value="0.0"/>
    <control-setting axis="/controls/gear/gear-down" value="1"/>
    <solve-weight idx="0" weight="0"/>
  </approach>

<!-- Cruise configuration -->
<!--  <cruise speed="504" alt="48000" fuel="0.3"> -->
  <cruise speed="520" alt="40000" fuel="0.3">
<!--  <cruise speed="449" alt="0" fuel="0.3"> -->
    <control-setting axis="/controls/engines/engine[0]/throttle" value="1.0"/>
    <control-setting axis="/controls/engines/engine[1]/throttle" value="1.0"/>
    <control-setting axis="/controls/flight/flaps" value="0.0"/>
    <control-setting axis="/controls/flight/spoilers" value="0.0"/>
    <control-setting axis="/controls/gear/gear-down" value="0"/>
    <solve-weight idx="0" weight="0"/>
  </cruise>

  <cockpit x="3.70" y="0.22" z="1.46"/>

<!-- Main Fuselage entry -->
<fuselage ax="0" ay="0.0" az="0.0" bx="-3.0" by="0" bz="0.3"
            width="1.9" taper="-0.1" midpoint="1"/>

  <fuselage ax="-3.3" ay="0.0" az="0.3" bx="-12.0" by="0" bz="0.3"
            width="2.0" taper="0" midpoint="0.4"/>
			
	<fuselage ax="-2.5" ay="0.3" az="1" bx="-5.0" by="0.3" bz="1"
            width="1.3" taper="0.3" midpoint="0.4"/>		
			
  <fuselage ax="-12.0" ay="0.0" az="0.3" bx="-19.5" by="0" bz="0.9"
            width="2.0" taper="0.1" midpoint="0.0"/>
			
<!-- Engines -->
	<fuselage ax="-5.2" ay="3.1" az="0.5" bx="-12.0" by="3.1" bz="0.2"
            width="1" taper="0.6" midpoint="0.2"/>	

<fuselage ax="-5.2" ay="-3.1" az="0.5" bx="-12.0" by="-3.1" bz="0.2"
            width="1" taper="0.6" midpoint="0.2"/>				

<!-- Wing -->
<mstab x="-9.00" y="0" z="0.15" incidence="6" twist="-2.30" taper="1"
        length="3.1" chord="6.00" sweep="0" dihedral="4.5" camber="0.0" >
    <stall aoa="20.00" width="2" peak="1.2"/>
<flap0 start="0.0" end="0.6" lift="1.7" drag="1.7"/>
 <flap1 start="0.28" end="1" lift="1.1" drag="7.5"/>
 <control-input axis="/controls/flight/flaps" control="FLAP0"/>
  <control-input axis="controls/flight/speedbrake" control="FLAP1"/>
 <control-output control="FLAP0" side="left" prop="/surface-positions/left-flap-pos-norm"/>
 <control-output control="FLAP0" side="right" prop="/surface-positions/right-flap-pos-norm"/>
 <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
  <control-output control="FLAP1" prop="/surface-positions/speedbrake-pos-norm"/>
  <control-speed control="FLAP0" transition-time="20"/>
  <control-speed control="FLAP1" transition-time="10"/>
 </mstab>


  <wing x="-9.00" y="3.1" z="0.45" incidence="2.30" twist="-2.30" taper="0.42"
        length="6.3" chord="6.00" sweep="-3.10" dihedral="4.5" camber="0.0">
    <stall aoa="20.00" width="2" peak="1.2"/>
   
    <flap0 start="0.0" end="0.6" lift="1.4" drag="1.3"/>
    <flap1 start="0.6" end="0.9" lift="1.2" drag="1.2"/>
    <spoiler start="0.4" end="0.6" lift="0.2" drag="4.0"/>

    <control-input axis="/controls/flight/flaps" control="FLAP0"/>
    <control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
    <control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
    <control-input axis="/controls/flight/spoilers" control="SPOILER"/>

    <control-output control="FLAP0" side="left" prop="/surface-positions/left-flap-pos-norm"/>
    <control-output control="FLAP0" side="right" prop="/surface-positions/right-flap-pos-norm"/>
    <control-output control="FLAP1" side="left" prop="/surface-positions/left-aileron-pos-norm"/>
    <control-output control="FLAP1" side="right" prop="/surface-positions/right-aileron-pos-norm"/>
    <control-output control="SPOILER" side="left" prop="/surface-positions/left-spoiler-pos-norm"/>
    <control-output control="SPOILER" side="right" prop="/surface-positions/right-spoiler-pos-norm"/>

    <control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
    <control-output control="FLAP1" prop="/surface-positions/aileron-pos-norm"/>
    <control-output control="SPOILER" prop="/surface-positions/spoiler-pos-norm"/>

    <control-speed control="FLAP0" transition-time="20"/>
    <control-speed control="FLAP1" transition-time="0.5"/>
    <control-speed control="SPOILER" transition-time="4.0"/>

  </wing>

<!-- HStab -->
  <hstab x="-17.85" y="0.36" z="0.80" taper="0.44"
         length="3.64" chord="2.91" sweep="8.5" dihedral="9.5"
         effectiveness="1.0" incidence="0.0">
    <stall aoa="20.0" width="3" peak="1.2"/>
    <flap0 start="0" end="1.2" lift="1.65" drag="1.5"/>

    <control-input axis="/controls/flight/elevator" control="FLAP0"/>
    <control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>

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

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

  </hstab>

<!-- Rudder -->
  <vstab x="-17.32" y="0" z="1.11" taper="0.42" effectiveness="1.0"
         length="2.36" chord="4.18" sweep="17">
    <stall aoa="28.0" width="3" peak="1.5"/>
    <flap0 start="0" end="1" lift="1.5" drag="1.4"/>

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

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

    <control-speed control="FLAP0" transition-time="1.0"/>

  </vstab>

<!-- Landing Gear -->



<!-- nose -->
  <gear x="-3.8" y="0" z="-1.50"
        compression="0.3" spring="1.5" damp="1.0">
    <control-input axis="/controls/flight/rudder" control="STEER" square="true"/>
    <control-input axis="/controls/gear/gear-down" control="EXTEND"/>
    <control-speed control="EXTEND" transition-time="12"/>
    <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
    <control-output control="STEER" prop="/gear/gear[0]/steering-norm"/>
  </gear>

<!-- left main -->
  <gear x="-8.11" y="2.5" z="-1.62"
        compression="0.5" spring="1.85" damp="2.0">
    <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="12"/>
    <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
  </gear>

<!-- right main -->
  <gear x="-8.11" y="-2.5" z="-1.62"
        compression="0.5" spring="1.85" damp="2.0">
    <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="12"/>
    <control-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
  </gear>

<!-- Engines -->
  <jet x="-6.10" y="3.10" z="0.47" mass="3000" thrust="7500" rotate="3.16">
    <actionpt x="-12.20" y="3.10" z="0.14"/>
    <control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
  </jet>

  <jet x="-6.10" y="-3.10" z="0.47" mass="3000" thrust="7500" rotate="3.16">
    <actionpt x="-12.20" y="-3.10" z="0.14"/>
    <control-input axis="/controls/engines/engine[1]/throttle" control="THROTTLE"/>
  </jet>

<!-- Fuel -->
<!-- Fuselage-->
  <tank x="-8.8" y="0.0" z="0.9" jet="true" capacity="6404"/>
<!-- Wings -->
  <tank x="-8.0" y="5.10" z="0.65" jet="true" capacity="5000"/>
  <tank x="-8.0" y="-5.10" z="0.65" jet="true" capacity="5000"/>
<!-- Tip tanks -->
  <tank x="-8.0" y="9.60" z="0.77" jet="true" capacity="1758"/>
  <tank x="-8.0" y="-9.60" z="0.77" jet="true" capacity="1758"/>

  <ballast x="-2.78" y="0" z="0.4" mass="3000"/> <!-- Cockpit/crew -->
  <ballast x="-5.12" y="0" z="0.2" mass="2000"/> <!-- avionics -->
  <ballast x="-6.0" y="0" z="-0.3" mass="3000"/> <!-- Trim ballast -->

<!-- Red Beard -->
  <weight x="-8.0" y="0" z="-0.10" size="0.9"
          mass-prop="/yasim/weights/red-beard-lbs"/>

</airplane>