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<p>Створена сторінка: Critical state and maximum effect of gyroscopic mounting appears when �� = 0. 5.3.2. Results and Analysis In Figure 16 the gyroscopic mounting effect on fre...</p> <p><b>Нова сторінка</b></p><div>Critical state and maximum effect of gyroscopic mounting appears when �� = 0. 5.3.2. Results and Analysis In Figure 16 the gyroscopic mounting effect on frequency jitter and phase noise is illustrated. According to this figure and Figure 5, this mounting shows its greatest advantages especially for the most probable crystals i.e., |��| [http://www.selleckchem.com/products/azd0156-azd-0156.html AZD-0156 nmr] respect to the distribution specified in Figure 5 for angle ��. Figure 17 Average instability caused by sinusoidal vibration. (a) Frequency jitter; (b) Phase noise. Table 5 Average efficiency of gyroscopic mounting for sinusoidal vibration. According to Figure 5, the gyro efficiency is shown in Figure 18 and Figure 19 and summarized in Table 6 and Table 7 for elevation angle |��| [http://www.selleckchem.com/products/cpi-0610.html Selleck CPI-0610] Allan deviation safety margin. (a) Fixed oscillator; (b) Gyroscopic mounting. Table 6 Analysis of gyroscopic mounting efficiency for crystal with |��| = 2.6��. Table 7 Analysis of gyroscopic mounting efficiency for crystal with |��| = 38��. According to Figure 18 and Figure 19 and Table 6, for a statistically minimum �� value i.e., �� = 2.6��, gyroscopic mounting has great effect and reduces frequency jitter [http://en.wikipedia.org/wiki/Ribosomal_s6_kinase S6 Kinase] close to the safety margin of the Allan deviation (10?4 Hz). For 2</div>

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