SIR deployment method with rough road immunity

• US 5,418,722 A
• Filed: 03/04/1994
• Issued: 05/23/1995
• Est. Priority Date: 03/04/1994
• Status: Expired due to Term

• Current Assignee: Loopback Technologies, Inc. (Marathon Patent Group, Inc.)
• Original Assignee: Delco Electronics Corporation (Motors Liquidation Co. GUC Trust)
• Inventors: Cashler, Robert J.
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): Walker, Tyrone V.
• Application Number:
  US08/205,464
• Time in Patent Office: 445 Days
• Field of Search: 364/424.05, 340/436, 340/669, 307/10.1, 280/734, 280/735, 180/282, 180/274
• US Class Current: 701/45
• CPC Class Codes: B60R 2021/01304 monitoring rough road condition
• CPC Class Codes: B60R 21/0132 responsive to vehicle motion parameters , e.g. to vehicle longitudinal or transversal deceleration or speed value
• CPC Class Codes: B60R 21/01336 using filtering

Abstract

A supplemental inflatable restraint system has a deployment algorithm which is enabled when a threshold acceleration is reached and then, based on subsequent measured acceleration data, determines whether and when to deploy an air bag. Rough road conditions produce accelerations which can enable the algorithm and then produce a reset event to terminate the algorithm. Reset events are each stored for a short time and the number of unexpired reset events is a measure of the rough road condition. The deployment calculation is adjusted to delay deployment for a time proportional to the number of reset events to allow gathering of additional acceleration data for the deployment decision.

Claims

1. A control method for deployment of a supplemental inflatable restraint in a motor vehicle comprising the steps of:

measuring vehicle acceleration;

initiating deployment calculation based on the measured acceleration when the measured acceleration exceeds a predetermined acceleration;

deploying the supplemental inflatable restraint when the deployment calculation indicates an occurrence of a crash event;

detecting a reset event indicative of a rough road condition;

terminating the deployment calculation when a reset event is detected prior to deploying the supplemental inflatable restraint;

storing a history of the detected reset events for a finite time; and

upon subsequent initiation of the deployment calculation, modifying such calculation in accordance with the history of detected reset events so as to prevent false deployment due to the rough road condition.

2. The invention as defined in claim 1 wherein the step of modifying the deployment calculation comprises delaying the deploying of the supplemental inflatable restraint to permit additional acceleration measurement for use in the deployment calculation.

3. The invention as defined in claim 1 wherein:

the step of storing a history of reset events comprises;

activating a reset indication of predetermined duration in response to each detected reset event; and

the step of modifying the deployment calculation comprises delaying the deploying of the supplemental inflatable restraint as a function of the number of active reset indications.

4. The invention as defined in claim 1 wherein:

the step of storing a history of reset events comprises activating a limited number of reset indications of predetermined duration in response to the most recently detected reset events; and

the step of modifying the deployment calculation comprises delaying the deploying of the supplemental inflatable restraint for a period which is proportional to the number of active reset indications.

5. The invention as defined in claim 3 including the step of deactivating the activated reset indications when the measured acceleration is indicative of a crash rather than rough road conditions.

6. The invention as defined in claim 3 including the step of deactivating the activated reset indications when the measured acceleration reaches a value significantly higher than acceleration values caused by rough road conditions.

7. The invention as defined in claim 3 including the steps of:

measuring the time elapsed after each deployment calculation initiation; and

deactivating the activated reset indications when the measured time becomes larger than a threshold time.

8. The invention as defined in claim 1 wherein the terminating step includes:

calculating an average acceleration from the measured acceleration;

repeatedly predicting a velocity for a given future time using the average acceleration;

and if at a preset point prior to the given future time the predicted velocity is below a preset threshold, terminating the deployment calculation.

9. The invention as defined in claim 1 wherein the terminating step includes:

calculating an average acceleration from the measured acceleration;

repeatedly predicting a velocity for a given future time using the average acceleration;

detecting peaks in the predicted velocity;

and if the predicted velocity drops below the last peak by a determined amount, terminating the deployment calculation.

10. The invention as defined in claim 1 wherein the terminating step includes:

filtering the measured acceleration;

and when the filtered acceleration attains a first threshold and then drops to a smaller threshold, terminating the deployment calculation.