def test_baro_pressure_at_10000m():
test_rocket = rm.Rocket()
test_rocket.baro = sensors.Baro_Pressure_Sensor()
test_rocket.temperature = -49.86
test_rocket.altitude = 10000
assert (abs(test_rocket.baro.update(test_rocket) - 26.5162) <=
rm.TOLERANCE)
def test_baro_pressure_at_ground():
test_rocket = rm.Rocket()
test_rocket.baro = sensors.Baro_Pressure_Sensor()
test_rocket.temperature = 15.04
test_rocket.altitude = 0
assert (abs(test_rocket.baro.update(test_rocket) - 101.4009) <=
rm.TOLERANCE)
def test_baro_pressure_at_20000m():
test_rocket = rm.Rocket()
test_rocket.baro = sensors.Baro_Pressure_Sensor()
test_rocket.temperature = -56.46
test_rocket.altitude = 20000
assert (abs(test_rocket.baro.update(test_rocket) - 5.5298) <= rm.TOLERANCE)