diff --git a/Aircraft-yasim/tsr2-yasim.xml b/Aircraft-yasim/tsr2-yasim.xml index 52c7823cf..eff4a26d2 100755 --- a/Aircraft-yasim/tsr2-yasim.xml +++ b/Aircraft-yasim/tsr2-yasim.xml @@ -2,103 +2,132 @@ representation of the aircraft. Having said that, the numbers, where I could find them, roughly match those of the original aircraft. Lee Elliott. + + The ailerons are a hack on this fdm - the real aircraft + use all moving tail planes for roll and this model had a + very high roll rate so they've been made relatively + ineffective and in the model/anim file the aileron surface + positions actually operate on the tailplanes. --> -<airplane mass="54750"> + <airplane mass="54750"> <!-- Approach configuration --> -<approach speed="180" aoa="6.0"> + <approach speed="130" aoa="10.0"> <control-setting axis="/controls/throttle[0]" value="0.2"/> - <control-setting axis="/controls/flaps" value="3.0"/> + <control-setting axis="/controls/throttle[1]" value="0.2"/> + <control-setting axis="/controls/flaps" value="1.0"/> + <control-setting axis="/controls/spoiler" value="0.2"/> <control-setting axis="/controls/gear-down" value="1"/> -</approach> + </approach> <!-- Cruise configuration --> <!-- <cruise speed="500" alt="35000"> --> -<cruise speed="800" alt="35000"> --> - <control-setting axis="/controls/throttle[0]" value="1.0"/> + <cruise speed="850" alt="35000"> --> + <control-setting axis="/controls/throttle[0]" value="0.95"/> + <control-setting axis="/controls/throttle[1]" value="0.95"/> <control-setting axis="/controls/flaps" value="0.0"/> <control-setting axis="/controls/gear-down" value="0"/> -</cruise> + </cruise> -<cockpit x="-4.5" y="0.0" z="1.0"/> + <cockpit x="8.5" y="0.0" z="1.0"/> -<fuselage ax="0" ay="0" az="0" bx="-27.13" by="0" bz=".64" + <fuselage ax="13.0" ay="0" az="0" bx="-14.13" by="0" bz=".64" width="2.0" taper="0.5" midpoint="0.3"/> -<wing x="-16.0" y="1.5" z="0" taper="0.25" - length="5.0" chord="6.0" sweep="50" dihedral="-1.0" camber="0.1"> - <stall aoa="3.0" width="5" peak="1.3"/> - <flap0 start="0.0" end="0.5" lift="2.0" drag="2.1"/> - <flap1 start="0.5" end="1.0" lift="1.15" drag="1.3"/> + <wing x="-3.0" y="1.5" z="1.7" taper="0.25" + length="5.0" chord="6.0" sweep="50" dihedral="-1.0" camber="0.003"> + <stall aoa="35.0" width="3" peak="1.3"/> + <flap0 start="0.0" end="0.9" lift="1.4" drag="1.2"/> + <flap1 start="0.0" end="0.4" lift="1.05" drag="1.2"/> + <spoiler start="0.54" end="0.86" lift="0.0" drag="20.0"/> + <control-input axis="/controls/flaps" control="FLAP0"/> <control-input axis="/controls/aileron" control="FLAP1" split="true"/> <control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/> + <control-input axis="/controls/spoilers" control="SPOILER"/> + <control-output control="FLAP0" prop="/surface-positions/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-speed control="FLAP0" transition-time="5"/> -</wing> + <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"/> -<hstab x="-23.0" y="-1.0" z="0.5" taper=".2" effectiveness="1.0" - length="3.0" chord="4.0" sweep="55" dihedral="-3.0"> - <stall aoa="3.0" width="10" peak="1.5"/> - <flap0 start="0" end="1" lift="1.7" drag="2.0"/> + <control-speed control="FLAP0" transition-time="5"/> + <control-speed control="SPOILER" transition-time="0.5"/> + + </wing> + + <hstab x="-10.0" y="1.0" z="0.5" taper=".2" effectiveness="2.0" + length="3.0" chord="4.0" sweep="55" dihedral="0.0"> + <stall aoa="35.0" width="3" peak="1.5"/> + <flap0 start="0" end="1" lift="1.26" drag="1.3"/> <control-input axis="/controls/elevator" control="FLAP0"/> <control-input axis="/controls/elevator-trim" control="FLAP0"/> <control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/> -</hstab> + </hstab> -<vstab x="-23.0" y="0" z="1.38" taper=".176" + <vstab x="-10.0" y="0" z="1.38" taper=".176" effectiveness="1.0" length="4.5" chord="4.0" sweep="50"> - <stall aoa="3.0" width="10" peak="1.5"/> + <stall aoa="28.0" width="3" peak="1.5"/> <flap0 start="0" end="1" lift="1.15" drag="1.3"/> <control-input axis="/controls/rudder" control="FLAP0" invert="true"/> <control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/> -</vstab> - -<jet x="-21.0" y="-1.0" z=".44" mass="4000" thrust="16600" afterburner="30600"> -<!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> --> - <control-input axis="/controls/throttle[0]" control="THROTTLE"/> - <control-input axis="/controls/afterburner[0]" control="REHEAT"/> -</jet> - -<jet x="-21.0" y="1.0" z=".44" mass="4000" thrust="16600" afterburner="30600"> -<!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> --> - <control-input axis="/controls/throttle[1]" control="THROTTLE"/> - <control-input axis="/controls/afterburner[1]" control="REHEAT"/> -</jet> + </vstab> <!-- nose --> -<gear x="-8.0" y="0" z="-1.93" retract-time="7" compression="1.3"> + <gear x="3.0" y="0" z="-2.0" retract-time="7" compression="0.8"> <control-input axis="/controls/rudder" control="STEER" square="true"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear/position-norm"/> -</gear> + </gear> <!-- left main --> -<gear x="-19.0" y="1.19" z="-1.56" retract-time="7" compression="0.2"> + <gear x="-4.0" y="1.19" z="-2.0" retract-time="7" compression="0.8"> <control-input axis="/controls/brakes[0]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/> -</gear> + </gear> <!-- right main --> -<gear x="-19.0" y="-1.19" z="-1.56" retract-time="7" compression="0.2"> + <gear x="-4.0" y="-1.19" z="-2.0" retract-time="7" compression="0.8"> <control-input axis="/controls/brakes[1]" control="BRAKE"/> <control-input axis="/controls/gear-down" control="EXTEND"/> <control-speed control="EXTEND" transition-time="7"/> <control-output control="EXTEND" prop="/gear/gear[1]/position-norm"/> -</gear> + </gear> -<tank x="-12.0" y="0" z="0.5" jet="true" capacity="11000"/> -<tank x="-13.0" y="0" z="0" jet="true" capacity="12000"/> -<tank x="-14.0" y="0" z="0" jet="true" capacity="12000"/> +<!-- Canopy --> + <gear x="3.0" y="0.0" z="0.6" retract-time="7" compression="0.6"> + <control-input axis="/controls/parking-brake" control="EXTEND"/> + <control-speed control="EXTEND" transition-time="10"/> + <control-output control="EXTEND" prop="/canopy/position-norm"/> + </gear> -<ballast x="-11.0" y="0" z="1" mass="1000"/> <!-- avionics --> + <jet x="-8.0" y="-1.0" z=".44" mass="4000" thrust="16600" afterburner="30600"> +<!-- <jet x="-22.0" y="-1.0" z=".44" mass="4000" thrust="30600"> --> + <control-input axis="/controls/throttle[0]" control="THROTTLE"/> + <control-input axis="/controls/afterburner[0]" control="REHEAT"/> + </jet> + + <jet x="-8.0" y="1.0" z=".44" mass="4000" thrust="16600" afterburner="30600"> +<!-- <jet x="-22.0" y="1.0" z=".44" mass="4000" thrust="30600"> --> + <control-input axis="/controls/throttle[1]" control="THROTTLE"/> + <control-input axis="/controls/afterburner[1]" control="REHEAT"/> + </jet> + + <tank x="-2.0" y="0.0" z="1.0" jet="true" capacity="13000"/> + <tank x="-3.0" y="2.5" z="1.7" jet="true" capacity="11000"/> + <tank x="-3.0" y="-2.5" z="1.7" jet="true" capacity="11000"/> + + <ballast x="8.5" y="0" z="0" mass="3000"/> <!-- Cockpit --> + <ballast x="4.0" y="0" z="0" mass="3000"/> <!-- avionics --> + <ballast x="-6.0" y="0" z="0" mass="100"/> <!-- Trim ballast --> </airplane> diff --git a/Aircraft/tsr2-yasim-set.xml b/Aircraft/tsr2-yasim-set.xml index 86713fa09..8a4f9e145 100755 --- a/Aircraft/tsr2-yasim-set.xml +++ b/Aircraft/tsr2-yasim-set.xml @@ -36,7 +36,7 @@ BAC TSR2 simulation config. <view n="1"> <config> - <z-offset-m type="double" archive="y">-70.0</z-offset-m> + <z-offset-m type="double" archive="y">-50.0</z-offset-m> </config> </view> @@ -52,20 +52,20 @@ BAC TSR2 simulation config. <config> <min-climb-speed-kt type="float">150.0</min-climb-speed-kt> - <best-climb-speed-kt type="float">500.0</best-climb-speed-kt> + <best-climb-speed-kt type="float">650.0</best-climb-speed-kt> - <target-climb-rate-fpm type="float">20000.0</target-climb-rate-fpm> - <target-descent-rate-fpm type="float">12000.0</target-descent-rate-fpm> + <target-climb-rate-fpm type="float">12000.0</target-climb-rate-fpm> + <target-descent-rate-fpm type="float">8000.0</target-descent-rate-fpm> - <elevator-adj-factor type="float">40.0</elevator-adj-factor> + <elevator-adj-factor type="float">400.0</elevator-adj-factor> <integral-contribution type="float">0.005</integral-contribution> - <max-aileron type="float">5.0</max-aileron> + <max-aileron type="float">0.3</max-aileron> <max-roll-deg type="float">60.0</max-roll-deg> <roll-out-deg type="float">8.0</roll-out-deg> - <roll-out-smooth-deg type="float">25.0</roll-out-smooth-deg> + <roll-out-smooth-deg type="float">8.0</roll-out-smooth-deg> <zero-pitch-throttle type="float">0.5</zero-pitch-throttle> <zero-pitch-trim-full-throttle type="float">0.001</zero-pitch-trim-full-throttle>