Error detection circuit for an airbag deployment control system

• US 6,559,557 B2
• Filed: 12/20/2000
• Issued: 05/06/2003
• Est. Priority Date: 12/20/2000
• Status: Expired due to Fees

• Current Assignee: Delphi Technologies, Inc. (BorgWarner Incorporated)
• Original Assignee: Delphi Technologies, Inc. (BorgWarner Incorporated)
• Inventors: Boger, Lee C., Manlove, Gregory J.
• Primary Examiner(s): Sircus, Brian
• Assistant Examiner(s): RIOS CUEVAS, ROBERTO JOSE
• Application Number:
  US09/742,792
• Publication Number:
  US 20020074859A1
• Time in Patent Office: 867 Days
• Field of Search: 307/9.1, 307/10.1, 701/45, 701/47, 701/46, 280/728.1, 180/282, 342/106
• US Class Current: 307/10.1
• CPC Class Codes: B60R 2021/01027 Safing sensors
• CPC Class Codes: B60R 2021/01177 Misdeployment, e.g. during assembly, disassembly, accident salvage or recycling
• CPC Class Codes: B60R 21/013 including means for detecting collisions, impending collisions or roll-over

Abstract

An error detection circuit for an airbag deployment control system includes a delay circuit receiving an analog acceleration signal, a difference circuit producing a difference signal based on a time difference between the original and delayed acceleration signals, and a first comparator circuit comparing the difference signal to first and second threshold signals. If the difference signal falls within an error region defined between the first and second threshold values, a decision circuit inhibits an otherwise pending airbag deployment event. If, on the other hand, the difference signal falls outside of the error region, the decision circuit allows airbag deployment with minimal delay. The error detection circuit further includes a second comparator circuit comparing the acceleration signal to near-supply and near-ground threshold values, wherein the decision circuit also inhibits airbag deployment if the acceleration signal magnitude exceeds the near-supply threshold value or falls below the near-ground threshold value.

Claims

1. An error detection circuit for an airbag deployment control system, comprising:

a delay circuit receiving an analog acceleration signal and producing a delay signal corresponding to said analog acceleration signal delayed in time;

a differential circuit subtracting said delay signal from said analog acceleration signal and producing a difference signal corresponding thereto; and

a first comparison circuit responsive to said difference signal to produce a first inhibit signal for inhibiting deployment of an airbag if said difference signal falls within a first predefined signal range.

2. The error detection circuit of claim 1 wherein said first comparison circuit is further responsive to said difference signal to allow deployment of said airbag if said difference signal falls outside said first predefined signal range.

3. The error detection circuit of claim 1 further including a first threshold signal circuit producing first and second threshold signals, said first and second threshold signals defining said first predefined signal range therebetween.

4. The error detection circuit of claim 3 wherein said first comparison circuit includes:

a first comparator responsive to said difference signal and said first threshold signal to produce a first comparator output signal;

a second comparator responsive to said difference signal and said second threshold signal to produce a second comparator output signal; and

a logic gate responsive to said first and second comparator output signals to produce said first inhibit signal.

5. The error detection circuit of claim 4 wherein said first and second threshold signals are each DC signals with said first threshold signal larger than said second threshold signal.

6. The error detection circuit of claim 4 wherein said first comparator includes a non-inverting input receiving said difference signal and an inverting input receiving said first threshold signal;

and wherein said second comparator includes an inverting input receiving said difference signal and a non-inverting input receiving said second threshold signal, said first threshold signal greater than said second threshold signal;

and wherein said logic gate is an OR gate.

7. The error detection circuit of claim 1 further including an accelerometer producing said analog acceleration signal.

8. The error detection circuit of claim 1 further including a second comparison circuit responsive to said analog acceleration signal to produce a second inhibit signal for inhibiting deployment of an airbag if said analog acceleration signal falls outside a second predefined signal range.

9. The error detection circuit of claim 8 further including a second threshold signal circuit producing third and fourth threshold signals, said third and fourth threshold signals defining said second predefined signal range therebetween.

10. The error detection circuit of claim 9 wherein said second comparison circuit includes:

a third comparator responsive to said analog acceleration signal and said third threshold signal to produce a third comparator output signal;

a fourth comparator responsive to said analog acceleration signal and said fourth threshold signal to produce a fourth comparator output signal; and

a logic gate responsive to said third and fourth comparator output signals to produce said second inhibit signal.

11. The error detection circuit of claim 10 wherein said third threshold signal corresponds to a predefined percentage of a supply voltage and said fourth threshold signals corresponds to a predefined voltage level above ground potential.

12. The error detection circuit of claim 10 wherein said third comparator includes a non-inverting input receiving said analog acceleration signal and an inverting input receiving said third threshold signal;

and wherein said fourth comparator includes an inverting input receiving said analog acceleration signal and a non-inverting input receiving said fourth threshold signal, said third threshold signal greater than said fourth threshold signal;

and wherein said logic gate is a NOR gate.

13. The error detection circuit of claim 8 further including an accelerometer producing said analog acceleration signal.

14. A method of inhibiting airbag deployment in an airbag deployment control system, the method comprising the steps of:

receiving an analog acceleration signal over time;

delaying said acceleration signal for a predefined time period and producing a delay signal corresponding thereto;

subtracting said delay signal from said analog acceleration signal and producing a difference signal corresponding thereto;

comparing said difference signal with a first signal window; and

inhibiting deployment of an airbag if said difference signal falls within said first signal window.

15. The method of claim 14 further including the steps of:

providing a first signal threshold;

providing a second signal threshold less then said first signal threshold; and

defining said first signal window as a range of signals between said first and second signal thresholds.

16. The method of claim 15 further including the steps of:

comparing said analog acceleration signal with a second signal window; and

inhibiting deployment of an airbag if said analog acceleration signal falls outside said second signal window.

17. The method of claim 16 further including the steps of:

providing a third signal threshold;

providing a fourth signal threshold less then said third signal threshold; and

defining said second signal window as a range of signals between said third and fourth signal thresholds.

18. The method of claim 17 wherein said third signal threshold is greater than said first signal threshold;

and wherein said fourth signal threshold is less than said second signal threshold.