You can not select more than 25 topics
Topics must start with a letter or number, can include dashes ('-') and can be up to 35 characters long.
267 lines
9.3 KiB
267 lines
9.3 KiB
<?xml version="1.0" encoding="UTF-8"?>
|
|
|
|
<!--
|
|
|
|
Normal rotor speed is 600 rpm with a Vmax of 1000 rpm,
|
|
and the blades have been tested up to 4000N static tensile strength,
|
|
with a maximum centrifugal load of five tons at 300 rpm in a 3-G pull-up maneuver.
|
|
|
|
Vne: 95 kts
|
|
Max Cruise: 80 kts
|
|
Economy Cruise: 70 kts
|
|
Best Climb: 52 kts
|
|
|
|
Rotor Diameter: 7 m
|
|
Rotorblade Chord:180 mm
|
|
Fuselage Length: 3.5 m
|
|
Height: 2.0 m
|
|
Wheel Track: 1.7 m
|
|
Propeller Diameter: 1.2 m
|
|
Rotor Disk Area: 38.5 sqm
|
|
Empty Weight: 167 kg
|
|
Gross Weight: 290 kg
|
|
Max Disc Loading: 7.5 kg/sqm
|
|
Max Power Loading: 3.9 kg/hp
|
|
Vne: 170 kmh
|
|
Max Cruise: 140 kmh
|
|
Economy Cruise: 120 kmh
|
|
Minimum Speed: 40 kmh
|
|
Max ROC: 3 m/s
|
|
Service Ceiling (estimated): 4000 m (13000 ft)
|
|
Takeoff Run 10 m
|
|
Landing Run: 5 m
|
|
Range: 250 km
|
|
|
|
-->
|
|
|
|
<airplane version="2018.1" mass-kg="3.2" mtow-kg="25">
|
|
|
|
<approach speed="20" aoa="0">
|
|
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.60"/>
|
|
</approach>
|
|
|
|
<cruise speed="26" alt="0">
|
|
<control-setting axis="/controls/engines/engine[0]/throttle" value="0.75"/>
|
|
</cruise>
|
|
|
|
<rotor name="main"
|
|
x="-0.24" y="0.0" z="0.33"
|
|
nx="0" ny="0" nz="1"
|
|
fx="1" fy="0" fz="0" ccw="1"
|
|
maxcollective="3.5" mincollective="3.5"
|
|
maxcyclicele="0" mincyclicele="0"
|
|
maxcyclicail="0" mincyclicail="0"
|
|
diameter="2.1"
|
|
numblades="2"
|
|
weightperblade="1.1"
|
|
twist="0"
|
|
chord="0.05"
|
|
rpm="700"
|
|
tiltcenterx="-0.24" tiltcentery="0" tiltcenterz="0.30"
|
|
mintiltpitch=" 2"
|
|
maxtiltpitch="22"
|
|
mintiltroll="-2"
|
|
maxtiltroll=" 2"
|
|
relbladecenter="0.7"
|
|
dynamic="1"
|
|
sharedflaphinge="0"
|
|
rellenflaphinge="0.0"
|
|
delta3="1"
|
|
delta="0.8"
|
|
pitch-a="6.3"
|
|
pitch-b="6.3"
|
|
flapmin="-8"
|
|
flapmax="8"
|
|
flap0="-3"
|
|
flap0factor="0"
|
|
notorque="0"
|
|
translift-ve="15"
|
|
translift-maxfactor="1"
|
|
ground-effect-constant="0.2"
|
|
taper="1"
|
|
number-of-segments="8"
|
|
number-of-parts="8"
|
|
rel-len-where-incidence-is-measured="0.5"
|
|
rel-len-blade-start="0.125"
|
|
airfoil-lift-coefficient="6.8"
|
|
airfoil-drag-coefficient0="0.0075"
|
|
airfoil-drag-coefficient1="0.325"
|
|
airfoil-incidence-no-lift="0"
|
|
incidence-stall-zero-speed="15"
|
|
incidence-stall-half-sonic-speed="14.5"
|
|
lift-factor-stall="0.6"
|
|
stall-change-over="10"
|
|
drag-factor-stall="1.5"
|
|
cyclic-factor="0.8"
|
|
rotor-correction-factor="0.95"
|
|
downwashfactor="0.0"
|
|
balance="0.999995"
|
|
>
|
|
<control-input axis="/controls/flight/aileron-trim" control="TILTROLL" split="true" src0="-1.0" src1="1.0" dst0="1.0" dst1="-1.0"/>
|
|
<control-input axis="/controls/flight/aileron" control="TILTROLL" src0="-1.0" src1="1.0" dst0="1.0" dst1="-1.0"/>
|
|
<control-input axis="/controls/flight/elevator-trim" control="TILTPITCH" split="true" src0="-1.0" src1="1.0" dst0="1.0" dst1="-1.0"/>
|
|
<control-input axis="/controls/flight/elevator" control="TILTPITCH" src0="-1.0" src1="1.0" dst0="1.0" dst1="-1.0"/>
|
|
|
|
</rotor>
|
|
<rotorgear max-power-engine="0.750"
|
|
max-power-rotor-brake="0.050"
|
|
rotorgear-friction="0.0005"
|
|
engine-prop-factor="0.02"
|
|
engine-accel-limit="5"
|
|
yasimdragfactor="30"
|
|
yasimliftfactor="140"
|
|
>
|
|
<!-- ROTORGEARENGINEON is unable to handle proportional input (https://sourceforge.net/p/flightgear/flightgear/ci/next/tree/src/FDM/YASim/Rotor.cpp#l1533)-->
|
|
<control-input axis="/controls/engines/engine[0]/starter" control="ROTORGEARENGINEON"/>
|
|
<control-input axis="/controls/rotor/brake" control="ROTORBRAKE" src0="0.0" src1="1.0" dst0="0.0" dst1="1.0"/>
|
|
</rotorgear>
|
|
|
|
<!-- Thruster device which does not produce adjacent moments-->
|
|
|
|
<thruster x="0" y="0" z="0.03" vx="1" vy="0" vz="0" thrust="6.61">
|
|
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE" src0="-1" src1="1" dst0="-1" dst1="1"/>
|
|
</thruster>
|
|
|
|
<!--
|
|
<propeller x="0.02" y="0" z="0.03"
|
|
mass="0.05"
|
|
moment="0.05"
|
|
radius="0.203"
|
|
cruise-speed="70"
|
|
cruise-rpm="2800"
|
|
cruise-alt="2000"
|
|
cruise-power="1"
|
|
takeoff-power="2"
|
|
takeoff-rpm="3600"
|
|
contra="1"
|
|
>
|
|
<actionpt x="0" y="0" z="0.03"/>
|
|
<piston-engine eng-power="2" eng-rpm="3800" displacement="20" >
|
|
<control-input axis="/controls/engines/engine[0]/throttle" control="THROTTLE"/>
|
|
<control-input axis="/controls/engines/engine[0]/starter" control="STARTER"/>
|
|
<control-input axis="/controls/engines/engine[0]/magnetos" control="MAGNETOS"/>
|
|
<control-input axis="/controls/engines/engine[0]/mixture" control="MIXTURE"/>
|
|
</piston-engine>
|
|
</propeller>
|
|
-->
|
|
|
|
|
|
<!-- main fuselage -->
|
|
<fuselage ax="0" ay="0" az="0" bx="-0.62" by="0" bz="0" width="0.2" taper="0" midpoint="0.25"/>
|
|
|
|
<!-- main tube -->
|
|
<fuselage ax="0" ay="0" az="0" bx="-0.92" by="0" bz="0" width="0.03" taper="1" midpoint="0.6"/>
|
|
|
|
<!-- gear tubes -->
|
|
<!--
|
|
<fuselage ax="-0.06838" ay="-0.15" az="-0.02754" bx="-0.06838" by="0.15" bz="-0.02754" width="0.03" taper="0" midpoint="0.5"/>
|
|
<fuselage ax="-0.41636" ay="-0.15" az="-0.02754" bx="-0.41636" by="0.15" bz="-0.02754" width="0.03" taper="0" midpoint="0.5"/>
|
|
-->
|
|
|
|
<hstab x="-0.91" y="0.0" z="0"
|
|
taper="1"
|
|
length="0.15"
|
|
chord="0.15"
|
|
sweep="0"
|
|
dihedral = "0"
|
|
>
|
|
<stall aoa="14" width="4" peak="1.5"/>
|
|
|
|
</hstab>
|
|
|
|
<vstab x="-0.91" y="0.15" z="-0.055"
|
|
chord="0.25"
|
|
length="0.15"
|
|
taper="1"
|
|
sweep="0"
|
|
incidence="0" >
|
|
<stall aoa="16" width="4" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.2" drag="0.8"/>
|
|
<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>
|
|
|
|
<vstab x="-0.91" y="-0.15" z="-0.055"
|
|
chord="0.25"
|
|
length="0.15"
|
|
taper="1"
|
|
sweep="0"
|
|
incidence="0" >
|
|
<stall aoa="16" width="4" peak="1.5"/>
|
|
<flap0 start="0" end="1" lift="1.2" drag="0.8"/>
|
|
<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>
|
|
|
|
<gear x="-0.06471" y="0.0" z="-0.205" compression="0.051">
|
|
<control-input axis="/controls/flight/rudder" control="STEER" square="false" src0="-1.0" src1="1.0" dst0="-0.3" dst1="0.3"/>
|
|
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true"/>
|
|
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
|
|
</gear>
|
|
|
|
<gear x="-0.34368" y="0.25" z="-0.205" compression="0.051">
|
|
<control-input axis="/controls/gear/brake-right" control="BRAKE" split="true"/>
|
|
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
|
|
</gear>
|
|
|
|
<gear x="-0.34368" y="-0.25" z="-0.205" compression="0.051">
|
|
<control-input axis="/controls/gear/brake-left" control="BRAKE" split="true"/>
|
|
<control-input axis="/controls/gear/brake-parking" control="BRAKE" split="true"/>
|
|
</gear>
|
|
|
|
<!-- tail gear -->
|
|
<gear x="-1.12" y="0.000" z="-0.09"
|
|
compression="0.08"
|
|
ignored-by-solver="1" >
|
|
</gear>
|
|
|
|
|
|
<!-- fuel tank for moddeled engine-->
|
|
<tank x="-0.1" y="0.0" z="-0.05" capacity="0.2"/>
|
|
|
|
<!-- rotor head ballast -->
|
|
<ballast x="-0.24" y="0.0" z="0.33" mass-kg="0.5"/>
|
|
|
|
<!-- gear weights and balasts -->
|
|
<!--
|
|
<weight x="-0.06471" y="0.225" z="-0.2" mass-prop="/sim/weight[0]/weight-kg"/>
|
|
<weight x="-0.06471" y="-0.225" z="-0.2" mass-prop="/sim/weight[1]/weight-kg"/>
|
|
<weight x="-0.34368" y="0.225" z="-0.2" mass-prop="/sim/weight[2]/weight-kg"/>
|
|
<weight x="-0.34368" y="-0.225" z="-0.2" mass-prop="/sim/weight[2]/weight-kg"/>
|
|
-->
|
|
|
|
<ballast x="-0.06471" y="0" z="-0.2" mass-kg="0.3"/>
|
|
<ballast x="-0.34368" y="0.225" z="-0.2" mass-kg="0.15"/>
|
|
<ballast x="-0.34368" y="-0.225" z="-0.2" mass-kg="0.15"/>
|
|
|
|
|
|
|
|
<!-- engine balast -->
|
|
<ballast x="0.0" y="0.0" z="0.02" mass-kg="0.7"/>
|
|
|
|
|
|
<!-- accumulator balasts -->
|
|
<ballast x="-0.15" y="0.1" z="0.0" mass-kg="0.25"/>
|
|
<ballast x="-0.15" y="-0.1" z="0.0" mass-kg="0.25"/>
|
|
|
|
|
|
<!-- tail balasts -->
|
|
<ballast x="-0.98" y="0.15" z="0.00" mass-kg="0.26"/>
|
|
<ballast x="-0.98" y="-0.15" z="0.00" mass-kg="0.26"/>
|
|
|
|
<!-- hitch -->
|
|
<hitch name="winch" x="0.0" y="0.0" z="0.0">
|
|
<tow length="50" weight-per-meter="0.0035" elastic-constant="40000" break-force="10000"/>
|
|
<!-- 3mm paracord-->
|
|
<winch max-tow-length="1000" min-tow-length="1" initial-tow-length="1000" max-winch-speed="20" power="2" max-force="80"/>
|
|
<control-input axis="/controls/winch/place" control="PLACEWINCH"/>
|
|
</hitch>
|
|
<hitch name="aerotow" x="0.0" y="0.0" z="0.0" force-is-calculated-by-other="0">
|
|
<tow length="60" weight-per-meter="0.0035" elastic-constant="9000" break-force="100" mp-auto-connect-period="0.0"/>
|
|
<winch max-tow-length="1000" min-tow-length="60" initial-tow-length="60"/>
|
|
<control-input axis="/controls/aerotow/find-aircraft" control="FINDAITOW"/>
|
|
</hitch>
|
|
|
|
</airplane>
|
|
|