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What is the range of an order of angular rate magnitude that gyros used in military planes need?(a) 8(b) 8.5(c) 7.1(d) 3I got this question in homework.This question is from Gyroscopes in portion Satellite Radio Navigation& Inertial Navigation of Avionics

Answer»

The correct answer is (b) 8.5

To EXPLAIN I would say: A gyroscope on a military AIRCRAFT must sense angular RATES as LOW as 0.005 deg/hr and as high as 400deg/sec, a RANGE of 8.5 orders of magnitude. Strapdown gyros in civil aircraft need only sense an 8 order of magnitude range of angular rates.



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