Duty-cycled gyroscope

Patent metadata

Field	Value
Publication number	US-10228249-B2
Application number	US-201615282227-A
Country	US
Kind code	B2
Filing date	Sep 30, 2016
Priority date	Mar 14, 2013
Publication date	Mar 12, 2019
Grant date	Mar 12, 2019

Abstract

A gyroscope system comprises a MEMS gyroscope coupled to a drive system and a sense system. The drive system maintains the MEMS gyroscope in a state of oscillation and the sense system for receiving, amplifying, and demodulating an output signal of the MEMS gyroscope that is indicative of the rate of rotation. The gyroscope system further includes a phase-locked look (PLL) which receives a reference clock (REFCLK) from the drive system and produces a system clock (CLK). Finally, the gyroscope system includes a controller operating on the system clock sets an operating state of the drive system and the sense system and also controls a state of the PLL. One or more system state variables are maintained in a substantially fixed state during a protect mode thereby enabling rapid transitions between a low-power mode and a normal operating mode of the gyroscope system.

First claim

What is claimed is:

1. A gyroscope duty-cycling method comprising:
operating a gyroscope in a low-power mode;
enabling a protection mode to maintain at least one system state variable in a substantially fixed state;
transitioning the gyroscope to a normal-power mode;
disabling the protection mode;
performing a measurement using the gyroscope;
enabling the protection mode to maintain the at least one system state variable in a substantially fixed state;
transitioning the gyroscope back to the low-power mode; and
disabling the protection mode.

2. The method of claim 1 , wherein the one or more system state variables comprise an automatic gain control (AGC) loop state variable or a Phase-Locked Loop (PLL) state variable.

3. The gyroscope system of claim 2 , wherein the AGC loop state variable comprises a gain control output voltage.

4. The gyroscope system of claim 2 , wherein the AGC loop state variable comprises a gain control output code.

5. The gyroscope system of claim 2 , wherein the PLL state variable comprises a voltage controlled oscillator (VCO) tuning voltage.

6. The gyroscope system of claim 2 , wherein the PLL state variable comprises an oscillator tuning code.

7. A method for duty-cycling a gyroscope system comprising:
enabling a protection mode of the gyroscope system, the protection mode being a mode wherein one or more system state variables are maintained in a substantially fixed state;
transitioning the gyroscope system between a normal power mode and a low power mode as needed; and
disabling the protection mode of the gyroscope subsequent to the transitioning.

8. The method of claim 7 , wherein once the protection mode is enabled, a drive system and/or a sense system of the gyroscope system makes a transition between the low-power mode and the normal operating mode without creating disturbances to the one or more system state variables.

9. The method of claim 7 , wherein the one or more system state variables comprise an automatic gain control (AGC) loop state variable and/or a Phase-Locked Loop (PLL) state variable.

10. The gyroscope system of claim 9 , wherein the AGC loop state variable comprises a gain control output voltage.

11. The gyroscope system of claim 9 , wherein the AGC loop state variable comprises a gain control output code.

12. The gyroscope system of claim 9 , wherein the PLL state variable comprises a voltage controlled oscillator (VCO) tuning voltage.

13. The gyroscope system of claim 9 , wherein the PLL state variable comprises an oscillator tuning code.

14. A method comprising:
disabling a sense path of a sense system of a gyroscope to operate the gyroscope in a low-power mode;
enabling a protection mode to maintain a state associated with a slow system state variables;
transitioning the gyroscope to a normal-power mode;
disabling the protection mode;
enabling the sense path of the sense system of the gyroscope; and
performing a measurement using the gyroscope.

15. The method of claim 14 further comprising:
enabling the protection mode to maintain the state associated with a slow system state variables;
transitioning the gyroscope to the low-power mode; and
disabling the protection mode.

16. The method of claim 14 , wherein the state is associated with automatic gain control (AGC) loop or tuning voltage of a voltage-controlled oscillator (VCO) of a phase-locked loop (PLL).

17. The method of claim 16 , wherein enabling the protection mode comprises:
disconnecting input of the AGC.

18. The method of claim 16 , wherein enabling the protection mode comprises:
preventing the PLL from responding to input clock edges.

19. The method of claim 16 , wherein enabling the protection mode comprises:
preventing input and output into and out of a loop filter of the PLL.

Assignees

• Invensense Inc

Inventors

• Shaeffer Derek
• Wang Stanley

Classifications

• H03L7/093

  using special filtering or amplification characteristics in the loop (H03L7/087 - H03L7/091 take precedence) · CPC title

• G01C19/5776 Primary

  Signal processing not specific to any of the devices covered by groups G01C19/5607 - G01C19/5719 · CPC title

• G01C19/10 Primary

  Power supply · CPC title

• G01C19/065

  Means for measuring or controlling of rotors' angular velocity · CPC title

• Y10T74/1229

  Gyroscope control · CPC title