Method and apparatus for providing location information
US-2015358778-A1 · Dec 10, 2015 · US
US9658338B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9658338-B2 |
| Application number | US-201213446744-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 13, 2012 |
| Priority date | Apr 13, 2012 |
| Publication date | May 23, 2017 |
| Grant date | May 23, 2017 |
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Official abstract text for this publication.
A device is disclosed that is capable of determining its location using high-power with high accuracy, and using low-power with lower accuracy. By coordinating usage between the high power method and the low power, overall power consumption of the device can be significantly reduced without a significant reduction in accuracy. Such high accuracy may be achieved through the use of a GNSS unit, such a GPS receiver. In addition, the low-power alternative may be achieved using an accelerometer, together with software, hardware or firmware for extrapolating a speed based on the force measurements by the accelerometer. In this manner, the GPS receiver can be operated for only a fraction of overall use, primarily to provide adjustment data necessary to calibrate usage of the accelerometer.
Opening claim text (preview).
What is claimed is: 1. A method for measuring a speed of a GNSS-enabled device, the method comprising: receiving force measurements from a force measurement module; and during a first operation state: operating a GNSS receiver in a high-power state; calculating a step length based on the force measurements received from the force measurement module and location information received from the GNSS receiver; storing the step length in a memory module; calculating the speed based on the location information received from the GNSS receiver; switching from the first operation state to a second operation state when a first predetermined time period has elapsed since the GNSS-enabled device entered the first operation state; and switching from the second operation state to the first operation state when: a second redetermined time period has elapsed since the GNSS-enabled device entered the second operation state; and the calculated speed has changed from a previously-calculated speed by more than a predetermined threshold. 2. The method of claim 1 , further comprising: during the second operation state: operating the GNSS receiver in a low-power state; and calculating the speed based on the force measurements received from the force measurement module and the stored step length. 3. The method of claim 2 , further comprising: during the first operation state: detecting a first force waveform from the force measurement module; and storing the first force waveform. 4. The method of claim 3 , further comprising: during the second operation state: detecting, by the force measurement module, a second force waveform; and performing pattern matching on the second force waveform to identify steps within the second force waveform. 5. The method of claim 4 , wherein the force measurement module is configured to detect force on a plurality of force axes, and wherein the second force waveform is detected on a first force axis of the plurality of force axes. 6. The method of claim 5 , further comprising: during the second operation mode: detecting, by the force measurement module, a third force waveform on a second force axis of the plurality of force axes, wherein the speed is calculated based on the third force waveform. 7. A GNSS-enabled device, comprising: a force measurement module configured to measure forces on the GNSS-enabled device; a GNSS receiver; and one or more processors and/or circuits configured to: receive the force measurements from the force measurement module; and during a first operation state: operate the GNSS receiver in a high-power state; calculate a step length based on the force measurements received from the force measurement module and location information received from the GNSS receiver; store the step length in a memory module; calculate the speed based on the location in formation received from the GNSS receiver; switch from the first operation state to a second operation state when a first predetermined time period has elapse since the GNSS-enabled device entered the first operation state; and switch from the second operation state to the first operation state when: a second predetermined time period has elapsed since the GNSS-enabled device entered the second operation state; and the calculated speed has changed from a previously-calculated speed by more than a predetermined threshold. 8. The GNSS-enabled device of claim 7 , wherein the one or more processors and/or circuits are further configured to: during the second operation state: operate the GNSS receiver in a low-power state; and calculate the speed based on the force measurements received from the force measurement module and the stored step length. 9. The GNSS-enabled device claim 8 , wherein the one or more processors and/or circuits are further configured to: during the first operation state: detect a first force waveform from the force measurement module; and store the first force waveform. 10. The GNSS-enabled device of claim 9 , wherein the one or more processors and/or circuits are further configured to: during the second operation state: detect, by the force measurement module, a second force waveform; and perform pattern matching on the second force waveform to identify steps within the second force waveform. 11. The GNSS-enabled device of claim 10 , wherein the force measurement module is configured to detect force on a plurality of force axes, and wherein the second force waveform is detected on a first force axis of the plurality of force axes. 12. The GNSS-enabled device of claim 11 , wherein the one or more processors and/or circuits are further configured to: during the second operation mode: detect, by the force measurement module, a third force waveform on a second force axis of the plurality of force axes, wherein the speed is calculated based on the third force waveform.
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