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feat(sihsim): more airplane thrust for a 30 deg climb and 20 m/s cruise
At 9000 RPM the propeller produced 4.6 N at trim airspeed while the model needs about 5.3 N to hold 15 m/s level, so the plane could not sustain trim airspeed at all. Spin the same APC 8x6" propeller at 13000 RPM, which gives 11.3 N at trim airspeed. The step is this large because prop wash over the tailplane and the fin increases their local dynamic pressure, which eats roughly three quarters of any added thrust. Also raise the maximum climb rate, since a 30 deg climb at trim airspeed needs 15 m/s * sin(30 deg) = 7.5 m/s and the default is 5 m/s. Measured in SITL: 19.7 m/s at full throttle in near level flight (3 deg, 1 m/s climb). The thrust sustains a climb of over 30 deg, but reaching it requires a steeper pitch than the takeoff and pitch limit defaults allow. Signed-off-by: Silvan <silvan@auterion.com>
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@@ -31,11 +31,16 @@ param set-default SIH_F_CP0 0.0777
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param set-default SIH_F_CP1 0.0498
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param set-default SIH_F_CP2 -0.11
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param set-default SIH_F_DIA_INCH 8
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param set-default SIH_F_RPM_MAX 9000
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param set-default SIH_F_RPM_MAX 13000
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param set-default SIH_VEHICLE_TYPE 1 # sih as fixed wing
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param set-default RWTO_TKOFF 1 # enable takeoff from runway (as opposed to launched)
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# 13000 RPM gives ~11 N of thrust at trim airspeed, which is a 30 deg climb at
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# trim and 20 m/s in level flight. Raise the climb rate so TECS
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# can command that climb (15 m/s * sin(30 deg) = 7.5 m/s)
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param set-default FW_T_CLMB_MAX 8
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param set-default CA_ROTOR_COUNT 1
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param set-default CA_ROTOR0_PX 0.3
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