发明名称 Phase locked loop control system gyroscope wheel speed control system - uses phase-locked loop having low response provided by frequency divider and low pass loop filter
摘要 <p>The phase-locked loop includes a h.f. (e.g. 20 MHz) crystal controlled voltage controlled oscillator (VCXO); a divider (33b) for dividing the VCXO frequency down (e.g. by six decades); a phase comparator (35) for comparing the output of the divider with a low frequency reference signal. A loop filter (37) is provided for filtering the output of the phase comparator so as to give the loop its desired dynamic response characteristic and bandwidth. A summing amplifier (39) sums the output of the phase comparator with a modulation signal. The arrangement controls the frequency of the power applied to a gyroscope to rotate the seismic mass (wheel) of the gyro so as to compensate for movement of the gyro case about the spin axis of the gyro, the modulation signal having a voltage level linearly related to the rate of movement of the gyro case about its spin axis. This signal is obtained from a second gyro mounted so as to sense movement about the spin axis of the gyro whose power frequency is being modulated.</p>
申请公布号 DE2907689(A1) 申请公布日期 1980.09.11
申请号 DE19792907689 申请日期 1979.02.27
申请人 THE BOEING CO. 发明人 R. OLBRECHTS,GUY
分类号 G01C19/06;(IPC1-7):05F1/00;01C19/06;05D13/62 主分类号 G01C19/06
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