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Operating method for a coriolis gyroscope and evaluation/adjustment electronic system and pulse modulator suitable therefor

一种脉冲调制器、运转方法的技术,应用在转向感应设备等方向,能够解决限制、使用大量电能、数字/模拟转换器大量供给电压等问题,达到制造成本低、少电能的效果

Inactive Publication Date: 2006-06-07
LITEF
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, it has the disadvantage that the electronics of the evaluation / control electronics are very complex
Thus, in figure 2 The embodiment of the Cortesian gyroscope shown has to use a large number of digital / analog converters (for example, at the points marked by reference numerals 26, 27 and 28), and these components are expensive and require a lot of power
Also, it should be noted that digital / analog converters often require large supply voltages and are difficult to integrate with other electronic components, especially digital ones, thus limiting the miniaturization of the implementation

Method used

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  • Operating method for a coriolis gyroscope and evaluation/adjustment electronic system and pulse modulator suitable therefor
  • Operating method for a coriolis gyroscope and evaluation/adjustment electronic system and pulse modulator suitable therefor
  • Operating method for a coriolis gyroscope and evaluation/adjustment electronic system and pulse modulator suitable therefor

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Embodiment Construction

[0063] figure 1 Shows evaluation / control electronics 30 with charge amplifier 31, analog / digital converter 32, demultiplexer 33, first demodulator 34, second demodulator 35, control system 36, two-dimensional pulse Modulator 37 , first and second force pulse conversion units 38 , 39 and first to fourth force transmitter electrodes 40 1 to 40 4 .

[0064] The overall scheme formed by the elements identified by reference numerals 31 to 40 comprises two control loops: one control loop for setting the amplitude / frequency of the excitation oscillation and another control return for setting the amplitude / frequency of the readout oscillation.

[0065] Such as figure 1 As shown, the circuit according to the present invention has only one analog / digital converter 32 and no digital / analog converter. In this solution the digital / analog converter is replaced by a two-dimensional pulse modulator 37 and two force pulse conversion units 38 , 39 .

[0066] The method of operating the e...

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Abstract

The invention relates to a method of operating a Cortex gyroscope (1), in which a digital readout signal is generated which indicates the instantaneous amplitude / frequency of the excitation / readout oscillations of a resonator (2) of the Cortex gyroscope (1). The resonator (2) has an energy signal input. The energy signal is conditioned based on the digital readout signal in such a way that the excitation / readout oscillations are assumed to have a specific amplitude / frequency. The energy signal (S3-S6) is generated from the quantized output signal (S1, S2) of the pulse modulator (37) which has as input a digital excitation / compensation signal (S15) derived from the digital readout signal (S9, S10). -S18).

Description

technical field [0001] The invention relates to a method of operating a Corian gyroscope, as well as evaluation / control electronics suitable for this purpose. Background technique [0002] Cortesian gyroscopes (also known as vibrating gyroscopes) are increasingly being used for navigation purposes. Coriolis gyroscopes have a system of masses that can be induced to oscillate. This oscillation is generally a superposition of multiple independent oscillations. These independent oscillations of the mass system are initially independent of each other, and each oscillation can be abstractly called a "resonator". The operation of the vibrating top requires at least two resonators: one of them (the first resonator) is artificially excited to oscillate, hereinafter referred to as "excited oscillation". The other resonator (second resonator) is excited to oscillate only when the vibrating top is moved / rotated. This is because in this case a Coriolis force occurs which connects the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C19/56
CPCG01C19/56
Inventor 冈特·斯帕林格
Owner LITEF
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