Duty-cycled gyroscope

Patent metadata

Field	Value
Publication number	US-9506757-B2
Application number	US-201314088059-A
Country	US
Kind code	B2
Filing date	Nov 22, 2013
Priority date	Mar 14, 2013
Publication date	Nov 29, 2016
Grant date	Nov 29, 2016

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 system comprising:
a MEMS gyroscope having a drive motion and producing an output signal proportional to a rate of rotation and to a velocity of the drive motion;
a drive system for regulating the drive motion;
a sense system for receiving the output signal and producing a demodulated output signal;
a phase-locked loop (PLL) for receiving a reference clock (REFCLK) from the drive system and producing a system clock (CLK); and
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, wherein 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.

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

3. The gyroscope system of claim 2 , wherein when the protect mode is enabled, the drive system and/or the sense system makes a transition between the low-power and the normal operating modes without creating disturbances to the one or more system state variables.

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

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

6. The gyroscope system of claim 3 , wherein the PLL state variable comprises a voltage controlled oscillator (VCO) tuning voltage.

7. The gyroscope system of claim 3 , wherein the PLL state variable comprises an oscillator tuning code.

Assignees

• Invensense Inc

Inventors

• Shaeffer Derek
• Wang Stanley

Classifications

• Y10T74/1229

  Gyroscope control · CPC title

• H03L7/093

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

• G01C19/065

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

• H03L7/099

  concerning mainly the controlled oscillator of the loop · CPC title

• H03G3/20

  Automatic control ({H03G3/005 takes precedence;} combined with volume compression or expansion H03G7/00) · CPC title