5deg/s is zero rate output over temperature which is not that bad but noise density of 0.12 deg/s/√Hz is two and half times bigger than ADXRS610 (0.05). The mechanical resonance is 10Khz.
Most importantly, the Data Sheet doesn't specify the internal vibration frequency - which is the first clue to where the harmonic-induced-error characteristics might compare to others. (perhaps it's important to note here, that the cost and performance of Gyro's is the single largest factor in the cost and performance of an IMU-flight controller - I'm pretty sure its important to know when a new gyro drops - and for those skilled in the art, a part number is equivalent to a hyper-link.)
Think of a new part (post) like a seed - you never know what will grow. (water nicely).
Yes, that's a bit confusing, but the picture is indeed linked. Normally on DIY Drones, clicking on the picture just brings up a larger picture, so I can understand why people would expect the same here. A tip for next time..
Comments
5deg/s is zero rate output over temperature which is not that bad but noise density of 0.12 deg/s/√Hz is two and half times bigger than ADXRS610 (0.05). The mechanical resonance is 10Khz.
Most importantly, the Data Sheet doesn't specify the internal vibration frequency - which is the first clue to where the harmonic-induced-error characteristics might compare to others. (perhaps it's important to note here, that the cost and performance of Gyro's is the single largest factor in the cost and performance of an IMU-flight controller - I'm pretty sure its important to know when a new gyro drops - and for those skilled in the art, a part number is equivalent to a hyper-link.)
Think of a new part (post) like a seed - you never know what will grow. (water nicely).