SYSTEM AND METHOD FOR AUTOMATIC MODAL PARAMETER EXTRACTION IN STRUCTURAL DYNAMICS ANALYSIS

• US 20130191071A1
• Filed: 01/17/2013
• Published: 07/25/2013
• Est. Priority Date: 01/23/2012
• Status: Abandoned Application

• Current Assignee: Airbus Group India Private Limited
• Original Assignee: Airbus Engineering Centre India Co.
• Inventors: MITRA, KAUSTAV
• Application Number:
  US13/743,333
• Publication Number:
  US 20130191071A1
• Time in Patent Office: Days
• US Class Current: 702/180
• CPC Class Codes: G01M 5/0025 of elongated objects, e.g. pipes, masts, towers or railways G01M5/0058 takes precedence
• CPC Class Codes: G01M 5/0066 by exciting or detecting vibration or acceleration vibration testing of structures G01M7/00
• CPC Class Codes: G01M 7/00 Vibration-testing of structures; Shock-testing of structures G01M9/00 takes precedence
• CPC Class Codes: G06F 17/18 for evaluating statistical data , e.g. average values, frequency distributions, probability functions, regression analysis forecasting specially adapted for a specific administrative, business or logistic context G06Q10/04

Abstract

A system and method for automatic modal parameter extraction in structural dynamics analysis are disclosed. In one embodiment, a stabilization diagram of a structure is obtained using a frequency domain parameter extraction technique. The stabilization diagram is a graph of measured transfer functions which include stable poles of the structure for each modal order versus frequencies which include modal frequencies of each stable pole. Further, a user is allowed to input user modal parameters, such as a maximum damping ratio, maximum number of stable poles to be selected from the stabilization diagram, and minimum separation in frequency between consecutive stable poles. Furthermore, stable poles having a damping ratio less than or equal to the maximum damping ratio are obtained. A histogram having bins, with a width equal to the minimum separation in frequency, is obtained. Also, the modal parameter of the structure is automatically extracted using the histogram.

Claims

1. A method of automatic modal parameter extraction in structural dynamics analysis, comprising:

obtaining a stabilization diagram of a structure using a frequency domain modal parameter extraction technique, wherein the stabilization diagram is a graph of measured transfer functions versus frequencies and wherein the measured transfer functions comprise stable poles of the structure for each modal order and the frequencies comprise modal frequencies of each of the stable poles;

allowing a user to input user modal parameters selected from the group consisting of a maximum damping ratio, a maximum number of stable poles to be selected from the stabilization diagram, and a minimum separation in frequency between consecutive stable poles;

obtaining stable poles having a damping ratio that is less than or equal to the maximum damping ratio from the stabilization diagram;

forming a histogram having bins, wherein each bin having a width approximately equal to the minimum separation in frequency between the consecutive stable poles; and

automatically extracting the modal parameter of the structure using the histogram.

2. The method of claim 1, wherein the structure is an aircraft structure, an automobile structure, a bridge structure, a building structure, an engine structure, and/or a brake disc structure.

3. The method of claim 1, wherein the modal parameter of the structure is selected from the group consisting of a natural frequency, a mode shape and a damping ratio.

4. The method of claim 1, wherein automatically extracting the modal parameter of the structure using the histogram comprises:

filtering out bins having no stable poles;

selecting remaining bins in a decreasing order of a number of stable poles in each of the remaining bins; and

extracting the modal parameter of the structure using the selected remaining bins.

5. The method of claim 4, wherein extracting the modal parameter of the structure using the selected remaining bins comprises:

calculating a distance parameter for each of the stable poles in one of the remaining bins;

calculating a first difference for each of the stable poles in the one of the remaining bins in an increasing order of frequency; and

selecting one of the stable poles having a minimum first difference in the one of the remaining bins.

6. The method of claim 5, further comprising:

repeating the steps of calculating the distance parameter, calculating the first difference and selecting a stable pole in a next bin of the remaining bins.

7. A modal parameter extraction system, comprising:

a processor; and

memory coupled to the processor, wherein the memory includes a modal parameter extraction tool having instructions to;

obtain a stabilization diagram of a structure using a frequency domain modal parameter extraction technique, wherein the stabilization diagram is a graph of measured transfer functions versus frequencies and wherein the measured transfer functions comprise stable poles of the structure for each modal order and the frequencies comprise modal frequencies of each of the stable poles;

allow a user to input user modal parameters selected from the group consisting of a maximum damping ratio, a maximum number of stable poles to be selected from the stabilization diagram, and a minimum separation in frequency between consecutive stable poles;

obtain stable poles having a damping ratio that is less than or equal to the maximum damping ratio from the stabilization diagram;

form a histogram having bins, wherein each bin has a width approximately equal to the minimum separation in frequency between the consecutive stable poles; and

automatically extract the modal parameter of the structure using the histogram.

8. The modal parameter extraction system of claim 7, wherein the structure is an aircraft structure, an automobile structure, a bridge structure, a building structure, an engine structure, and/or a brake disc structure.

9. The modal parameter extraction system of claim 7, wherein the modal parameter of the structure is selected from the group consisting of a natural frequency, a mode shape and a damping ratio.

10. The modal parameter extraction system of claim 7, wherein the modal parameter extraction tool further having instructions to:

filter out bins having no stable poles;

select remaining bins in a decreasing order of a number of stable poles in each of the remaining bins; and

extract the modal parameter of the structure using the selected remaining bins.

11. The modal parameter extraction system of claim 10, wherein the modal parameter extraction tool further having instructions to:

calculate a distance parameter for each of the stable poles in one of the remaining bins;

calculate a first difference for each of the stable poles in the one of the remaining bins in an increasing order of frequency; and

select one of the stable poles having a minimum first difference in the one of the remaining bins.

12. The modal parameter extraction system of claim 11, the modal parameter extraction tool further having instructions to:

repeat the steps of calculating the distance parameter, calculating the first difference and selecting a stable pole in a next bin of the remaining bins.

13. At least one non-transitory computer-readable storage medium for automatic modal parameter extraction in structural dynamics analysis having instructions that, when executed by a computing device, cause the computing device to:

obtain a stabilization diagram of a structure using a frequency domain parameter extraction technique, wherein the stabilization diagram is a graph of measured transfer functions versus frequencies, wherein the measured transfer functions comprise stable poles of the structure for each modal order and the frequencies comprise modal frequencies of each of the stable poles;

allow a user to input user modal parameters selected from the group consisting of a maximum damping ratio, a maximum number of stable poles to select from the stabilization diagram, and a minimum separation in frequency between consecutive stable poles;

obtain stable poles having a damping ratio that is less than or equal to the maximum damping ratio;

form a histogram having bins, wherein bin has a width approximately equal to the minimum separation in frequency between the consecutive stable poles; and

automatically extract the modal parameter of the structure using the histogram.

14. The at least one non-transitory computer-readable storage medium of claim 13, wherein the structure is an aircraft structure, an automobile structure, a bridge structure, a building structure, an engine structure, and/or a brake disc structure.

15. The at least one non-transitory computer-readable storage medium of claim 13, wherein the modal parameter of the structure is selected from the group consisting of a natural frequency, a mode shape and a damping ratio.

16. The at least one non-transitory computer-readable storage medium of claim 13, wherein automatically extracting the modal parameter of the structure using the histogram comprises:

filtering out bins having no stable poles;

selecting remaining bins in a decreasing order of a number of stable poles in each of the remaining bins; and

extracting the modal parameter of the structure using the selected remaining bins.

17. The at least one non-transitory computer-readable storage medium of claim 16, wherein extracting the modal parameter of the structure using the selected remaining bins comprises:

calculating a parameter for each of the stable poles in one of the remaining bins using distance of the stable pole in a hypothetical plane;

calculating a first difference for each of the stable poles in the one of the remaining bins in an increasing order of frequency; and

selecting one of the stable poles having a minimum first difference in the one of the remaining bins.

18. The at least one non-transitory computer-readable storage medium of claim 17, further comprising:

repeating the steps of calculating the parameter, calculating the first difference and selecting a stable pole in a next bin in the remaining bins.