IP Library › Granted Patent US 10,399,524
Granted Patent B2
US 10,399,524 · App. 16/080,190 · Granted Sep 3, 2019

Method for determining an impact intensity

Inventors: Marcus Gross (Farmington Hills, MI); Christian Ohl (Pfullingen, DE); Elvira Lehr (Northville Township, MI); Hans-Joerg Faisst (Kirchentellinsfurt, DE); Michael Roelleke (Leonberg-Hoefingen, DE); Josefine Ladda (Suzhou, CN); Stefan Schuster (Esslingen, DE)
Assignee: Robert Bosch GmbH
B60R21/0132G08B25/009G08B25/016B60R2021/0027B60R2021/01325G08B25/08
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Quick Facts
Patent No.
US 10,399,524
App. No.
16/080,190
Filed
Aug 27, 2018
Granted
Sep 3, 2019
Kind
B2
Art Unit
2689
USPC
340/436
Abstract

A method for generating a signal representing an impact intensity including the steps: receiving at least three signals, which represent respectively accelerations in different spatial directions; calculating a direction-independent variable from the three signals; ascertaining an integrated measurand of the direction-independent variable over a time window; generating a signal representing an impact intensity on the basis of the ascertained integrated measurand.

Claims (41)

1. A method for a vehicle for generating a signal representing an impact intensity, comprising:

receiving at least three signals, which represent respectively accelerations in different spatial directions;

calculating a direction-independent variable from the three signals;

adapting the direction-independent variable by subtracting a value representing gravitational acceleration from the direction-independent variable;

ascertaining an integrated measurand of the direction-independent variable over a time window; and

generating a signal representing an impact intensity from the ascertained integrated measurand.

2. The method as recited in claim 1 , wherein the three signals are low-pass filtered.

3. The method as recited in claim 1 , wherein the integrated measurand is ascertained continuously.

4. The method as recited in claim 1 , wherein the integrated measurand is compared to a predefined threshold value.

5. The method as recited in claim 1 , wherein a transmitting device is activated for transmitting the signal representing an impact intensity to: (i) an external receiving device, and/or (ii) a mobile terminal.

6. The method as recited in claim 1 , wherein the integrated measurand is ascertained continuously at a discrete-time sampling rate.

7. The method as recited in claim 1 , wherein a transmitting device is triggered based on the comparison to transmit the signal representing the impact intensity to at least one of: an external receiving device, or a mobile terminal.

8. A non-transitory machine-readable storage medium on which is stored a computer program for generating a signal representing an impact intensity, the computer program, when executed by a processor, causing the processor to perform:

receiving at least three signals, which represent respectively accelerations in different spatial directions;

calculating a direction-independent variable from the three signals;

adapting the direction-independent variable by subtracting a value representing gravitational acceleration from the direction-independent variable;

ascertaining an integrated measurand of the direction-independent variable over a time window; and

generating a signal representing an impact intensity from the ascertained integrated measurand.

9. An electronic control unit for generating a signal representing an impact intensity, the electronic control unit designed to:

receive at least three signals, which represent respectively accelerations in different spatial directions;

calculate a direction-independent variable from the three signals;

adapting the direction-independent variable by subtracting a value representing gravitational acceleration from the direction-independent variable;

ascertain an integrated measurand of the direction-independent variable over a time window; and

generate a signal representing an impact intensity from the ascertained integrated measurand.

10. A device, comprising:

an electronic control unit for generating a signal representing an impact intensity, the electronic control unit designed to:

receive at least three signals, which represent respectively accelerations in different spatial directions,

calculate a direction-independent variable from the three signals,

adapting the direction-independent variable by subtracting a value representing gravitational acceleration from the direction-independent variable;

ascertain an integrated measurand of the direction-independent variable over a time window, and

generate a signal representing an impact intensity from the ascertained integrated measurand; and

a triaxial acceleration sensor to detect the accelerations in the three different spatial directions.

11. The device as recited in claim 10 , further comprising:

a transmitting device to transmit the signal representing an impact intensity to: (i) an external receiving device, and/or (ii) a mobile terminal.

12. The device as recited in claim 11 , wherein the electronic control unit, the triaxial acceleration sensor, and the transmitting device are situated together in a common housing.

13. A method for a vehicle for generating a signal representing an impact intensity, comprising:

receiving at least three signals, which represent respectively accelerations in different spatial directions;

adapting at least one of the three signals by subtracting a value representing gravitational acceleration from the at least one of the three signals;

calculating a direction-independent variable from the three signals;

ascertaining an integrated measurand of the direction-independent variable over a time window; and

generating a signal representing an impact intensity from the ascertained integrated measurand.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 28, 2019
From: GROSS, MARCUS; OHL, CHRISTIAN; LEHR, ELVIRA; FAISST, HANS-JOERG; ROELLEKE, MICHAEL; LADDA, JOSEFINE; SCHUSTER, STEFAN
To: ROBERT BOSCH GMBH
Reel/Frame 048153/0393 →
Priority Claims (1)
DE 10 2016 205 545 · Apr 4, 2016 · national
Continuity (1)
Related Publication 20190054879A1 · Feb 21, 2019
Cited By (5)
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