Comment by Dano on April 1, 2011 at 6:22pm
Comment by Kirby on April 1, 2011 at 8:04pm
Comment by Joe Bloeski on April 1, 2011 at 11:41pm
Comment by Belli Button on April 1, 2011 at 11:49pm
Comment by bGatti on April 2, 2011 at 5:59am
Comment by bGatti on April 2, 2011 at 6:03am
Comment by Dano on April 2, 2011 at 10:06am
Comment by bGatti on April 2, 2011 at 6:27pm 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).
Comment by Sergiu on April 2, 2011 at 8:57pm 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.
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Season Two of the Trust Time Trial (T3) Contest has now begun. The third round was a reliablilty/aerial photography round for both planes and copters, which is now closed. Stay tuned for the next round, beginning soon.61 members
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