Method and apparatus for managing multiple sensors in a navigation system
US-8972180-B1 · Mar 3, 2015 · US
US9372097B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9372097-B2 |
| Application number | US-201214008835-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 24, 2012 |
| Priority date | Mar 30, 2011 |
| Publication date | Jun 21, 2016 |
| Grant date | Jun 21, 2016 |
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A rotational rate sensor is provided having a substrate and a Coriolis element, the rotational rate sensor having a drive means for exciting the Coriolis element to a Coriolis oscillation, and the rotational rate sensor having a detection device for producing a sensor signal as a function of a deflection of the Coriolis element relative to the substrate on the basis of a Coriolis force acting on the Coriolis element, and in addition the rotational rate sensor being configured to carry out a self-calibration when a rotational acceleration signal produced as a function of the sensor signal falls below a specified threshold value.
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What is claimed is: 1. A rotational rate sensor, comprising: a substrate; a Coriolis element; a driver to excite the Coriolis element to a Coriolis oscillation; a detection device to produce a sensor signal as a function of a deflection of the Coriolis element relative to the substrate based on a Coriolis force acting on the Coriolis element; wherein the rotational rate sensor is configured to carry out a self-calibration when a rotational acceleration signal produced as a function of the sensor signal falls below a threshold value; and a difference value formation unit configured to produce the rotational acceleration signal from a difference between at least two sensor values of the sensor signal. 2. The rotational rate sensor as recited in claim 1 , further comprising: a comparator to compare the rotational acceleration signal to the threshold value. 3. The rotational rate sensor as recited in claim 1 , further comprising: a differentiator that is configured to produce the rotational acceleration signal from a mathematical derivative of the sensor signal. 4. The rotational rate sensor as recited in claim 1 , further comprising: an intermediate storage device configured to store a multiplicity of sensor values of the sensor signal during execution of the self-calibration, the intermediate storage device being configured to store a sum of the multiplicity of sensor values of the sensor signal during the execution of the self-calibration. 5. The rotational rate sensor as recited in claim 4 , further comprising: a mean value formation unit configured to produce a new sensor offset value from a mathematical mean value of the sensor values stored in the intermediate storage device; and an offset storage device configured to store a sensor offset calculated as a function both of the new sensor offset value and of an earlier sensor offset value. 6. The rotational rate sensor as recited in claim 1 , further comprising: an interrupt interface, the rotational rate sensor being configured to produce an interrupt signal at the interrupt interface at least one of during and at a time after the execution of the self-calibration. 7. A method for calibrating a rotational rate sensor, the rotational rate sensor including a substrate, a Coriolis element, a driver to excite the Coriolis element to a Coriolis oscillation, a detection device to produce a sensor signal as a function of a deflection of the Coriolis element relative to the substrate based on a Coriolis force acting on the Coriolis element, wherein the rotational rate sensor is configured to carry out a self-calibration when a rotational acceleration signal produced as a function of the sensor signal falls below a threshold value, and a difference value formation unit configured to produce the rotational acceleration signal from a difference between at least two sensor values of the sensor signal, the method comprising: exciting the Coriolis element to the Coriolis oscillation; producing the sensor signal as a function of a deflection of the Coriolis element relative to the substrate on the basis of a Coriolis force acting on the Coriolis element; producing the rotational acceleration signal as a function of the sensor signal, wherein the rotational acceleration signal is the difference between the at least two sensor values of the sensor signal; and carrying out a self-calibration of the rotational rate sensor when it is detected that the rotational acceleration signal has fallen below a specified threshold value. 8. The method as recited in claim 7 , wherein the self-calibration is started when the rotational acceleration signal falls below the threshold value for a specified time span. 9. The method as recited in claim 7 , wherein the rotational acceleration signal is produced from a mathematical derivative of the sensor signal. 10. The method as recited in claim 7 , wherein for the self-calibration of the rotational rate sensor, a multiplicity of sensor values of the sensor signal are recorded, a sum of the sensor values being stored, and a new sensor offset value being calculated from the sensor values as a function of a mathematical mean value, a sensor offset being calculated both as a function of the new sensor offset value and as a function of an old sensor offset value. 11. The method as recited in claim 10 , wherein the self-calibration is terminated when, during the self-calibration, it is detected that the rotational acceleration signal has exceeded the specified threshold value.
initial alignment, calibration or starting-up of inertial devices · CPC title
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each sensing mass being connected to a driving mass, e.g. driving frames · CPC title
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