Motor = ACMotor()
Motor.name = 'Hyperion_ZS4020'
Motor.Battery = ThunderPower_4Cell_5000
Motor.Ri = 0.058*OHM #Coil resistance
Motor.Io = 1.4*A #Idle current
Motor.Kv = 585*RPM/V #RPM/Voltage ratio
Motor.Vmax = 25.9*V
Motor.Imax = 85*A
Motor.ThrustUnit = LBF
Motor.ThrustUnitName = 'lbf'
Motor.xRm = 1000000
Motor.Pz = 0.0
Motor.Weight = 304*GRAM*gacc
Motor.LenDi = [60.2*MM, 48.9*MM]
Arm=10.5*IN
Arm2=19.5*IN
#
# This data has been corrected for standard day
#
# RPM, Torque Current Voltage
STD = STDCorrection(30.29*inHg, (9.4 + 273.15)*K)
STD2 = STDCorrection(30.29*inHg, (9.8 + 273.15)*K)
STD3 = STDCorrection(30.25*inHg, (12 + 273.15)*K)
STD4 = STDCorrection(30.2*inHg, (6.667 + 273.15)*K)
STD5 = STDCorrection(30.31*inHg, (-9 + 273.15)*K)
TestData = [(6759 *RPM, (11.1*Arm*OZF)*STD, 53.62*A, 14.8*V),
(7097 *RPM, (9.8*Arm*OZF)*STD, 42.7*A, 14.8*V),
(6973 *RPM, (12.35*Arm*OZF)*STD, 54.51*A, 14.8*V),
(7104 *RPM, (9.78*Arm*OZF)*STD, 43.18*A, 14.8*V),
# Motor.Kv = 250*RPM/V #RPM/Voltage ratio
#Matched Data
Motor.Ri = 0.037 * OHM
Motor.Io = 0.69 * A
Motor.Kv = 250 * RPM / V
#
Motor.Vmax = 23.5 * V
Motor.Imax = 65 * A
Motor.ThrustUnit = LBF
Motor.ThrustUnitName = 'lbf'
Motor.xRm = 100000
Motor.Pz = 0.0
Motor.Weight = 450 * GRAM * gacc
Motor.LenDi = [48.8 * MM, 64.9 * MM]
# Assign objects to weight classes
Motor.Battery.WeightGroup = 'Electronics'
Motor.SpeedController.WeightGroup = 'Electronics'
Motor.WeightGroup = 'Propulsion'
#
# This data has been corrected for standard day
STD = STDCorrection(30.2 * inHg, (16.1 + 273.15) * K)
Arm = 19.5 * IN
# RPM, Torque Current Voltage
TestData = [(6030 * RPM, (7.3 * Arm * OZF) * STD, 32.0 * A, 22.8 * V),
(5670 * RPM, (8.3 * Arm * OZF) * STD, 36.0 * A, 22.2 * V),
(5430 * RPM, (9.3 * Arm * OZF) * STD, 39.5 * A, 21.5 * V),
# Motor.Kv = 300*RPM/V #RPM/Voltage ratio
#Matched data
Motor.Ri = .12 * OHM
Motor.Io = .5 * A
Motor.Kv = 355 * RPM / V
Motor.Vmax = 23.5 * V
Motor.Imax = 55 * A
Motor.ThrustUnit = LBF
Motor.ThrustUnitName = 'lbf'
Motor.xRm = 100000
Motor.Pz = 0.0
Motor.Weight = 445 * GRAM * gacc
Motor.LenDi = [46.8 * MM, 59.98 * MM]
#
# This data has been corrected for standard day
STD = STDCorrection(29.9 * inHg, (23.9 + 273.15) * K)
Arm = 19.5 * IN
# RPM, Torque Current Voltage
TestData = [(6210 * RPM, (7.5 * Arm * OZF) * STD, 34.8 * A, 23.0 * V),
(5910 * RPM, (8.7 * Arm * OZF) * STD, 39.0 * A, 21.9 * V),
(5610 * RPM, (9.9 * Arm * OZF) * STD, 44.2 * A, 21.5 * V),
(5640 * RPM, (9.3 * Arm * OZF) * STD, 40.5 * A, 21.4 * V)
] #this is actual test data from a test stand
Motor.TestData = TestData
if __name__ == '__main__':
# Motor.Kv = 320*RPM/V #RPM/Voltage ratio
# Matched Data
Motor.Ri = 0.037 * OHM # .15
Motor.Io = .69 * A # 1.5
Motor.Kv = 250 * RPM / V # 370
#
Motor.Vmax = 41.53 * V
Motor.Imax = 65 * A
Motor.ThrustUnit = LBF
Motor.ThrustUnitName = 'lbf'
Motor.xRm = 100000
Motor.Pz = 0.0
Motor.Weight = 450 * GRAM * gacc
Motor.LenDi = [46.8 * MM, 64.9 * MM]
#
# This data has been corrected for standard day
STD = STDCorrection(30.2 * inHg, (16.1 + 273.15) * K)
# RPM, Torque Current Voltage
TestData = [(2072 * RPM, (47 * IN * OZF) * STD, 7.2 * A, 24.44 * V),
(2730 * RPM, (81 * IN * OZF) * STD, 22.0 * A, 23.24 * V),
(3182 * RPM, (132 * IN * OZF) * STD, 38.4 * A, 22.05 * V),
(3659 * RPM, (200 * IN * OZF) * STD, 38.7 * A, 21.1 * V),
(4414 * RPM, (331 * IN * OZF) * STD, 50.9 * A, 21.31 * V)
] # this is actual test data from a test stand
1
Motor.TestData = TestData
if __name__ == '__main__':
