mirror of https://github.com/ArduPilot/ardupilot
59 lines
1.4 KiB
JSON
59 lines
1.4 KiB
JSON
# 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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