A simple and efficient approach for tuning finite element models to match computed frequencies, mode shapes, and mass properties to the experimental data is introduced in this study. The model tuning procedure proposed in this study is based on a series of optimizations. This approach has been successfully applied to create an equivalent beam finite element model for the X-37 drogue chute test fixture with the X-planes pylon. The goal was a simple model capable of being analyzed in a captive carry configuration with the B-52H mother ship. This study has shown that natural frequencies, corresponding mode shapes, and mass properties from the updated finite element model achieved at the final optimization iteration have excellent agreement with corresponding measured data.

1.
Baruch
,
M.
, and
Bar-Itzhack
,
I. Y.
, 1978, “
Optimal Weighted Orthogonalization of Measured Modes
,”
AIAA J.
0001-1452,
16
(
4
), pp.
346
351
.
2.
Minas
,
C.
, and
Inman
,
D. J.
, 1990, “
Matching Finite Element Models to Modal Data
,”
ASME J. Vibr. Acoust.
0739-3717,
112
, pp.
84
92
.
3.
Berman
,
A.
, and
Nagy
,
E. J.
, 1983, “
Improvement of a Large Analytical Model Using Test Data
,”
AIAA J.
0001-1452,
21
(
8
), pp.
1168
1173
.
4.
Schwarz
,
B.
,
Richardson
,
M.
, and
Formenti
,
D. L.
, 2007, “
FEA Model Updating Using SDM
,”
Sound Vib.
0038-1810,
41
(
10
), pp.
18
23
.
5.
Heylen
,
W.
, and
Vanhonacker
,
P.
, 1983, “
An Automated Technique for Improving Model Matrices by Means of Experimentally Obtained Dynamic Data
,” Paper No. AIAA-83-0881.
6.
Juneja
,
V.
,
Haftka
,
R. T.
, and
Cudney
,
H. H.
, 1994, “
Location of Damage in a Space Structure by Contrast Maximization
,” Paper No. AIAA-94-1711-CP.
7.
Kim
,
H. M.
, and
Bartkowicz
,
T. J.
, 1993, “
Damage Detection and Health Monitoring of Large Space Structures
,”
Sound Vib.
0038-1810,
27
(
6
), pp.
12
17
.
8.
Zimmerman
,
D. C.
, and
Simmermacher
,
T.
, 1994, “
Model Refinement and System Health Monitoring Using Data From Multiple Static Loads and Vibration Tests
,” Paper No. AIAA-94-1714-CP.
9.
Jaishi
,
B.
, and
Ren
,
W.-X.
, 2006, “
Damage Detection by Finite Element Model Updating Using Modal Flexibility Residual
,”
J. Sound Vib.
0022-460X,
290
(
1–2
), pp.
369
387
.
10.
Avitabile
,
P.
, 2003, “
Twenty Years of Structural Dynamic Modification—A Review
,”
Sound Vib.
0038-1810,
37
(
1
), pp.
14
27
.
11.
Chen
,
G.
, 2001, “
FE Model Validation for Structural Dynamics
,” Ph.D. thesis, Mechanical Engineering Department, University of London, London.
12.
Friswell
,
M. I.
, and
Mottershead
,
J. E.
, 1996,
Finite Element Model Updating in Structural Dynamics
,
Kluwer
,
Dordrecht
.
13.
Vanderplaats
,
G. N.
, 2001,
DOT User’s Manual Version 5.00
,
VR&D Engineering
,
Colorado Springs, CO
.
14.
Guyan
,
R. J.
, 1965, “
Reduction of Stiffness and Mass Matrices
,”
AIAA J.
0001-1452,
3
(
2
), p.
380
.
15.
O’Callahan
,
J. C.
, 1989, “
A Procedure for an Improved Reduced System (IRS) Model
,”
Seventh International Modal Analysis Conference
,
Las Vegas, NV
, Jan., pp.
17
21
.
16.
Reymond
,
M.
, and
Miller
,
M.
, 1996,
MSC/NASTRAN Quick Reference Guide Version, 69
,
The MacNeal-Schwendler Corporation
,
Los Angeles, CA
.
17.
Dong
,
S. B.
,
Wolf
,
J. A.
, and
Peterson
,
F. E.
, 1972, “
On a Direct-Iterative Eigensolution Technique
,”
Int. J. Numer. Methods Eng.
0029-5981,
4
, pp.
155
162
.
18.
Military Standard
, 1994, “
Test Requirements for Launch, Upper-Stage, and Space Vehicles, MIL-STD-1540C
,” Sec. 6.2.10, Sept. 15.
19.
Norton
,
W. J.
, 1990,
Structures Flight Test Handbook
,
Air Force Flight Test Center
,
Edwards, CA
, AFFTC-TIH-90-001.
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