Reference Oscillator Low-Power Timekeeping for GNSS Receivers

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Solution Overview

Problem

Existing clock circuits in digital electronic equipment, particularly in GNSS receivers, face challenges in maintaining a reliable time reference during low-power modes due to high power consumption, additional board space, and limited precision of auxiliary real-time clocks, which hinder efficient reacquisition of satellite signals after idle periods.

Innovation Solution

A reference oscillator circuit with a crystal resonator, temperature compensation, and a counter that switches between normal and low-power states to conserve power while maintaining time accuracy, allowing the circuit to store and retrieve elapsed time during idle periods, thereby enabling quick reacquisition of satellite signals.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If an auxiliary real-time clock (RTC) with a separate crystal resonator is used to keep time during low-power mode, then the receiver can maintain time reference during idle periods, but the board space is increased and the precision is limited

Engineering Contradiction:
Improvetime reference availabilityVSAvoidboard space
Core Design Contradiction:
ReliabilityVSArea of stationary object

Solution Approach 1:

The patent combines the time-keeping function with the existing main oscillator circuit by adding a counter that accumulates clock cycles during low-power mode. This eliminates the need for a separate RTC crystal resonator and its associated circuitry, thereby reducing board space while maintaining time reference availability. The counter stores the elapsed time in low-power mode, which is then used to calculate the wake-up time and enable quick reacquisition of satellite signals.

Inventive Principle:
Principle #5Merging (Combining)

2Reliability

If an auxiliary real-time clock (RTC) is used to keep time during low-power mode, then the receiver can maintain time reference, but the precision is limited and shock-sensitivity increases

Engineering Contradiction:
Improvetime reference availabilityVSAvoidtime reference precision
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The main oscillator circuit is designed to serve dual purposes: providing the primary time reference during normal operation and enabling time-keeping during low-power mode through the counter mechanism. By making the main oscillator multi-functional, the system eliminates the need for a separate, lower-precision RTC oscillator, thereby maintaining high time reference precision even during idle periods.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Use of energy by moving object

If the receiver switches to low-power mode to conserve battery, then power consumption is reduced, but the time reference becomes less accurate and reacquisition is delayed

Engineering Contradiction:
Improvepower consumptionVSAvoidreacquisition time
Core Design Contradiction:
Use of energy by moving objectVSLoss of time

Solution Approach 1:

The counter continuously accumulates clock cycles even during low-power mode, preparing the elapsed time information in advance. When the receiver wakes up, this pre-calculated time information is immediately available, allowing the system to quickly determine the current time and resume satellite signal acquisition without delay. This preliminary accumulation of time data during low-power periods eliminates reacquisition delays.

Inventive Principle:
Principle #10Preliminary action

4Measurement precision

If a high-precision quartz oscillator is used for the RTC, then time reference precision is improved, but the device cost increases appreciably

Engineering Contradiction:
Improvetime reference precisionVSAvoiddevice cost
Core Design Contradiction:
Measurement precisionVSEase of manufacture

Solution Approach 1:

The system uses its own main high-precision oscillator to serve the time-keeping function during low-power mode, rather than requiring a separate RTC oscillator. The counter accumulates cycles from the existing main oscillator, allowing the system to self-service its time-keeping needs without additional precision components, thereby avoiding increased device cost while maintaining high time reference precision.

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This solution reduces power consumption and eliminates the need for an auxiliary real-time clock, providing a reliable and precise time reference for GNSS receivers, allowing for immediate reacquisition of satellite signals upon waking from low-power mode, thus optimizing power management and reducing system complexity.

Implementation Method 1

a crystal resonator, having a resonance frequency; an oscillator circuit arranged to maintain the resonator in oscillation at the resonance frequency

Methodology Applied
Scientific EffectResonance: Resonance

Implementation Method 2

a temperature compensation circuit, providing a temperature-compensated clock output signal

Methodology Applied
Scientific EffectTemperature compensation:

Data Source

PatentEP1998451B1Reference oscillator and its use in a GNSS receiver
Publication Date: 2011.07.27 QUALCOMM INC
  • EP1998451B1 patent drawingFigure 1~2

AI summary

A reference clock circuit (170), has a low-power mode, in which the frequency consumption is reduced, and including an internal counter (100), accumulating time spent in low-power mode. The circuit includes a crystal resonator (60), an oscillator circuit (70), and a temperature compensation circuit (80), providing a stable clock output (85). During low-power mode temperature compensation can be switched off. The circuit further provides a wakeup signal (107) after a preset time in low-power mode. The reference clock circuit may be used in a GPS or GNSS receiver having an idle mode during which satellite tracking is not carried out and the reference circuit (170) is put into low-power mode. Time elapsed in the idle mode is retrieved from the internal counter (100) and used to resume acquisition and tracking of satellites.