Good Bye Andino
Posted: Wed Nov 11, 2015 10:41 pm
Thanks for all the hard work and the beautiful models you left behind.
All very appreciated.
A best wish,
IH-COL
All very appreciated.
A best wish,
IH-COL
An independent forum for FlightGear users and developers
https://thejabberwocky-net.brendtandbrendt.com/
https://thejabberwocky-net.brendtandbrendt.com/viewtopic.php?f=15&t=168
Andino wrote:By this communication I would like to let you know, that I am no longer able to continue developing the Airbus A340-600HGW, the A340-313X, the Boeing 707-320 and the MD-81, MD-82, and MD-83.
These models can still be downloaded from the website (https://andinogonthaeler.wordpress.com/), but they will not be developed further by me in a systematic way. If I occasionally do something new, I will let you know in the forum and in the blog, but not much work should be expected.
Due to personal reasons, I have not the time needed to work any more on these planes. And the pace of new FG versions is too quick for me to be able to do the necessary adjustments to each version.
As far as I know, models A340-600HGW, A340-313X and B-707-320 are completely under the GPL license. The MD's are under the Creative Commons license, as they are derived from the original MD-81, which was under the Creative Commons license. More is explained under each plane. Feel free to continue the work on these models.
Thank you for your support and interest so far.
Andino
Code: Select all
<!-- A340-313X Yasim by Andino
Information taken from:
http://www.airbus.com/aircraftfamilies/passengeraircraft/a340family/a340-300/specifications/
http://en.wikipedia.org/wiki/Airbus_A340
http://www.jet-engine.net/civtfspec.html
http://easa.europa.eu
http://www.aircraftenginedesign.com/TableB3.html
http://www.cfmaeroengines.com/engines/cfm56-5c
-->
<airplane mass="287000" version="YASIM_VERSION_CURRENT">
<approach speed="132" alt="0.0" aoa="5.0" fuel="0.2" glide-angle="0.0">
<control-setting axis="/controls/engines/engine[0]/throttle-act" value="0.25"/>
<control-setting axis="/controls/engines/engine[1]/throttle-act" value="0.25"/>
<control-setting axis="/controls/engines/engine[2]/throttle-act" value="0.25"/>
<control-setting axis="/controls/engines/engine[3]/throttle-act" value="0.25"/>
<control-setting axis="/controls/flight/flaps" value="1"/>
<control-setting axis="/surface-positions/slats" value="1"/>
<control-setting axis="/controls/gear/gear-down" value="1"/>
<solve-weight idx="0" weight="360"/>
<solve-weight idx="1" weight="42072"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="500" alt="35000" fuel="0.7">
<control-setting axis="/controls/engines/engine[0]/throttle-lever" value="0.75"/>
<control-setting axis="/controls/engines/engine[1]/throttle-lever" value="0.75"/>
<control-setting axis="/controls/engines/engine[2]/throttle-lever" value="0.75"/>
<control-setting axis="/controls/engines/engine[3]/throttle-lever" value="0.75"/>
<control-setting axis="/controls/flight/flaps" value="0.0"/>
<control-setting axis="/controls/gear/gear-down" value="0"/>
<solve-weight idx="0" weight="350"/>
<solve-weight idx="1" weight="45000"/>
</cruise>
<cockpit x="30.0" y="0.0" z="0.75"/>
<!--cockpit-->
<fuselage ax="32.34" ay="0" az="-0.64" bx="21.11" by="0.00" bz="0.0"
width="6.2" taper="0.0" midpoint="1.0" cx="2.4"/>
<fuselage ax="21.11" ay="0" az="-0.37" bx="-9.64" by="0.00" bz="-0.37"
width="6.2" taper="1.0" midpoint="0.5" cy="12.0" cz="12.0"/>
<fuselage ax="-9.64" ay="0" az="-0.37" bx="-34.0" by="0.00" bz="1.2"
width="6.2" taper="0.0" midpoint="0.0" cy="40.0" cz="40.0"/>
<!-- engines in fuselage -->
<fuselage ax="11.0" ay="9.8" az="-3" bx="6.2" by="9.8" bz="-3"
width="2.8" taper="1.0"/>
<fuselage ax="11.0" ay="-9.8" az="-3" bx="6.2" by="-9.8" bz="-3"
width="2.8" taper="1.0"/>
<fuselage ax="4.0" ay="20.7" az="-2" bx="-0.8" by="20.7" bz="-2"
width="2.8" taper="1.0"/>
<fuselage ax="4.0" ay="-20.7" az="-2" bx="-0.8" by="-20.7" bz="-2"
width="2.8" taper="1.0"/>
<!--surfaces-->
<wing x="3.5" y="3.0" z="-1.66" length="30.0" chord="11.0" sweep="25"
taper=".13" dihedral="7" camber="0.005" incidence="2.6" twist="-1">
<stall aoa="15" width="8" peak="1.5"/>
<flap0 start="0" end=".56" lift="1.5" drag="1.7"/>
<flap1 start=".64" end=".88" lift="1.5" drag="1.2"/>
<slat start="0" end="1" aoa="2" drag="1.2"/>
<spoiler start="0.2" end="0.6" lift="0.2" drag="3.0"/>
<control-input axis="/controls/flight/flaps" control="FLAP0"/>
<control-input axis="/surface-positions/flap-pos-norm" control="SLAT"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
<control-output control="FLAP0" prop="/surface-positions/slats"/>
<control-speed control="FLAP0" transition-time="10"/>
<control-input axis="/controls/flight/speedbrake" control="SPOILER"/>
<control-output control="SPOILER" prop="/surface-positions/speedbrake-norm"/>
<control-speed control="SPOILER" transition-time="5"/>
<control-input axis="/controls/flight/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/flight/aileron-trim" control="FLAP1" split="true"/>
<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"/>
</wing>
<hstab x="-25.16" y="1.5" z="1.36"
chord="5.5"
length="9.3"
taper="0.40"
effectiveness="1.4"
sweep="28"
dihedral="7">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.54" drag="1.2"/>
<control-input axis="/controls/flight/elevator" control="FLAP0"/>
<control-input axis="/controls/flight/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
</hstab>
<vstab x="-24.0" y="0.00" z="2.7" chord="8.0" length="10.2" taper="0.5"
sweep="33">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.2"/>
<control-input axis="/controls/flight/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"
min="1" max="-1"/>
</vstab>
<!-- Engines performance: CFM56-5C4 -->
<jet x="2.16" y="19.89" z="-1.995"
mass="5216"
thrust="34000"
spool-time="3"
egt="975"
tsfc="0.33"
epr="32.8"
exhaust-speed="1300.0"
n1-idle="45"
n1-max="105"
n2-idle="70"
n2-max="108">
<control-input axis="/controls/engines/engine[0]/throttle-lever" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[0]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[0]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="9.89" z="-2.995"/>
</jet>
<jet x="8.16" y="9.89" z="-2.995"
mass="5216"
thrust="34000"
spool-time="3"
egt="975"
tsfc="0.33"
epr="32.8"
exhaust-speed="1300.0"
n1-idle="45"
n1-max="105"
n2-idle="70"
n2-max="108">
<control-input axis="/controls/engines/engine[1]/throttle-lever" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[1]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[1]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[1]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="9.89" z="-2.995"/>
</jet>
<jet x="8.16" y="-9.89" z="-2.995"
mass="5216"
thrust="34000"
spool-time="3"
egt="975"
tsfc="0.33"
epr="32.8"
exhaust-speed="1300.0"
n1-idle="45"
n1-max="105"
n2-idle="70"
n2-max="108">
<control-input axis="/controls/engines/engine[2]/throttle-lever" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[2]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[2]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[2]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="-9.89" z="-2.995"/>
</jet>
<jet x="2.16" y="-19.89" z="-1.995"
mass="5216"
thrust="34000"
spool-time="3"
egt="975"
tsfc="0.33"
epr="32.8"
exhaust-speed="1300.0"
n1-idle="45"
n1-max="105"
n2-idle="70"
n2-max="108">
<control-input axis="/controls/engines/engine[3]/throttle-lever" control="THROTTLE"/>
<control-input axis="/controls/engines/engine[3]/mixture" control="MIXTURE"/>
<control-input axis="/controls/engines/engine[3]/reverser" control="REVERSE_THRUST"/>
<control-output control="REVERSE_THRUST" prop="/surface-positions/reverser-norm[3]"/>
<control-speed control="REVERSE_THRUST" transition-time="1.5"/>
<actionpt x="-2.7" y="-9.89" z="-2.995"/>
</jet>
<thruster x="19.28" y="0.00" z="-5.55" vx="1" vy="0" vz="0" thrust="25000">
<control-input axis="/sim/model/pushback/target-speed-fps" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
</thruster>
<!-- Gear-->
<!-- nose -->
<gear x="29.28" y="0.00" z="-5.55"
compression="0.6" spring="0.9" damp="1">
<!--control-input axis="/controls/flight/rudder" control="STEER" square="true"/-->
<control-input control="STEER" axis="/controls/gear/nosegear-steering-cmd-norm" src0="-1.0" dst0="-1.2217304764" src1="1.0" dst1="1.2217304764" />
<control-output control="STEER" prop="/controls/gear/nosegear-steering-angle-rad" />
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- Central-->
<gear x="-2.39" y="5.6" z="-5.7" compression="0.8" spring="1.0" >
<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-output control="EXTEND" prop="/gear/gear[1]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-2.39" y="-5.6" z="-5.7" compression="0.8" spring="1.0">
<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-output control="EXTEND" prop="/gear/gear[2]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<gear x="-2.39" y="0" z="-5.7" compression="3.0" spring="1.2" >
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[3]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- fake gear to simulate tail strikes -->
<gear x="-20.8" y="0" z="-5.7" compression="3.0" spring="1.2">
<control-input axis="/controls/gear/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[4]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
</gear>
<!-- Fuel. Max Capacity 39060 USG -->
<tank x="0" y="5" z="-1.5" jet="true" capacity="68400"/>
<tank x="1.0" y="0" z="-2.5" jet="true" capacity="125735"/>
<tank x="0" y="-5" z="-1.5" jet="true" capacity="68400"/>
<!-- Weight and ballast -->
<weight x="25.0" y="0" z="0" mass-prop="/sim/weight[0]/weight-lb"/>
<weight x="0.5" y="0" z="0" mass-prop="/sim/weight[1]/weight-lb"/>
<weight x="0.5" y="0" z="0" mass-prop="/sim/weight[2]/weight-lb"/>
<ballast x="-25" y="0" z="4" mass="-37000"/>
</airplane>