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58 lines
1.4 KiB
58 lines
1.4 KiB
# Callisto model, see https://www.freespaceoperations.com.au/ |
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{ |
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# total vehicle mass |
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"mass" : 32.5, |
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# vehicle diameter |
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"diagonal_size" : 1.325, |
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# the ref parameters should be taken from a test |
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# with the copter flying at constant speed in zero wind. This is used |
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# to estimate the drag coefficient |
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"refSpd" : 14.88, # m/s |
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"refAngle" : 8.91, # degrees |
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"refVoltage" : 46.9, # volts |
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"refCurrent" : 65.36, # Amps |
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"refAlt" : 26, # meters AMSL |
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"refTempC" : 25, # degrees C |
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"refBatRes" : 0.024, # BAT.Res from log |
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# full battery voltage |
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"maxVoltage" : 50.4, |
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# full battery capacity, Ah |
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"battCapacityAh" : 44, |
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# MOT_THST_EXPO |
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"propExpo" : 0.5, |
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# approximage maximum yaw rate in deg/sec |
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"refRotRate" : 120, |
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# hover throttle from 0 to 1 |
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"hoverThrOut" : 0.36, |
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# MOT_PWM_MIN |
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"pwmMin" : 1000, |
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# MOT_PWM_MAX |
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"pwmMax" : 1940, |
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# MOT_SPIN_MIN |
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"spin_min" : 0.2, |
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# MOT_SPIN_MAX |
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"spin_max" : 0.975, |
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# maximum motor slew rate, or zero to disable |
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"slew_max" : 75, |
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# total effective disc area in sq m for 4 x 30 inch diameter rotors |
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# coaxial rotors count as a single rotor for this parameter) |
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"disc_area" : 1.82, |
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# momentum drag coefficient |
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# ratio of momentum drag realtive to a ducted rotor of the same effective disc area |
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"mdrag_coef" : 0.10 |
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}
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