发明名称 Slow acting phase-locked loop with external control signal
摘要 A modulator for controlling 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 is disclosed. The modulator includes a slow acting phase-locked loop that includes: a high frequency (e.g., 20 MHz) crystal controlled voltage controlled oscillator (VCXO); a divider for dividing the VCXO frequency down by several orders of magnitude (e.g., six); a phase comparator for comparing the relatively low frequency output of the divider with a low frequency reference signal; a loop filter for filtering the output of the phase comparator so as to give the loop its desired dynamic response chacteristic and bandwidth; and, a summing amplifier for summing the output of the phase comparator with a rate signal having a voltage level linearly related to the rate of movement of the gyro case about its spin axis. The rate 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. The power frequency control signal is derived from the output of the VCXO via a divider, which may form part of the divider of the slow acting phase-locked loop.
申请公布号 US4382234(A) 申请公布日期 1983.05.03
申请号 US19790088295 申请日期 1979.10.26
申请人 THE BOEING COMPANY 发明人 OLBRECHTS, GUY R.
分类号 G01C19/04;H03C3/09;(IPC1-7):H03L7/08 主分类号 G01C19/04
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