| Year |
Citation |
Score |
| 2012 |
Peterson LD. New millennium program space technology 8: Validation through modeling and test Journal of Spacecraft and Rockets. 49: 969. DOI: 10.2514/1.60038 |
0.325 |
|
| 2007 |
Silver MJ, Peterson LD, Hardaway LMR. Experimental Measurement of Picometer Scale Spontaneous Vibrations in a Precision Deployable Boom under Thermal Loading Shock and Vibration. 14: 133-149. DOI: 10.1155/2007/393578 |
0.354 |
|
| 2006 |
Lake MS, Peterson LD, Mikulas MM. Space structures on the back of an envelope: John Hedgepeth's design approach Journal of Spacecraft and Rockets. 43: 1174-1183. DOI: 10.2514/1.21076 |
0.693 |
|
| 2005 |
Silver MJ, Peterson LD, Erwin RS. Predictive elastothermodynamic damping in finite element models by using a perturbation formulation Aiaa Journal. 43: 2646-2653. DOI: 10.2514/1.12329 |
0.341 |
|
| 2005 |
Hinkle J, Peterson L, Klein K, Levine M, Peng C. Submicron friction mechanics at ambient and cryogenic temperatures Proceedings of Spie. 5899: 589910. DOI: 10.1117/12.626173 |
0.395 |
|
| 2005 |
Peterson LD, Hinkle JD. What limits the achievable areal densities of large aperture space telescopes? Proceedings of Spie - the International Society For Optical Engineering. 5899: 1-12. DOI: 10.1117/12.619878 |
0.479 |
|
| 2002 |
Lake MS, Peterson LD, Levine MB. Rationale for Defining Structural Requirements for Large Space Telescopes Journal of Spacecraft and Rockets. 39: 674-681. DOI: 10.2514/2.3889 |
0.451 |
|
| 2002 |
Hinkle JD, Warren P, Peterson LD. Geometric Imperfection Effects in an Elastically Deployable Isogrid Column Journal of Spacecraft and Rockets. 39: 662-668. DOI: 10.2514/2.3887 |
0.427 |
|
| 2002 |
Heald JC, Peterson LD. Deployment repeatability of a space telescope reflector petal Journal of Spacecraft and Rockets. 39: 771-779. DOI: 10.2514/2.3878 |
0.532 |
|
| 2002 |
Domber JL, Hinkle JD, Peterson LD, Warren PA. Dimensional Repeatability of an Elastically Folded Composite Hinge for Deployed Spacecraft Optics Journal of Spacecraft and Rockets. 39: 646-652. DOI: 10.2514/2.3877 |
0.609 |
|
| 2002 |
Hardaway LMR, Peterson LD. Nanometer Scale Spontaneous Vibrations In A Deployable Truss Under Mechanical Loading Aiaa Journal. 40: 2070-2076. DOI: 10.2514/2.1540 |
0.386 |
|
| 1999 |
Hachkowski MR, Peterson LD, Lake MS. Friction model of a revolute joint for a precision deployable spacecraft structure Journal of Spacecraft and Rockets. 36: 591-598. DOI: 10.2514/3.27205 |
0.351 |
|
| 1999 |
Warren PA, Peterson LD, Hinkle JD. Submicron Mechanical Stability of a Prototype Deployable Space Telescope Support Structure Journal of Spacecraft and Rockets. 36: 765-771. DOI: 10.2514/2.3492 |
0.524 |
|
| 1999 |
Bullock SJ, Peterson LD. Nanometer Regularity in the Mechanics of a Precision Deployable Spacecraft Structure Joint Journal of Spacecraft and Rockets. 36: 758-764. DOI: 10.2514/2.3491 |
0.408 |
|
| 1998 |
Alvin KF, Peterson LD. Determination of Modal Residues and Residual Flexibility for Time-Domain System Realization Journal of Guidance Control and Dynamics. 21: 588-594. DOI: 10.2514/2.4298 |
0.34 |
|
| 1998 |
Denoyer KK, Peterson LD. Comparing Model Update Error Residuals and Effects on Model Predictive Accuracy Aiaa Journal. 36: 1894-1900. DOI: 10.2514/2.283 |
0.319 |
|
| 1998 |
Doebling SW, Peterson LD, Alvin KF. Experimental Determination of Local Structural Stiffness by Disassembly of Measured Flexibility Matrices Journal of Vibration and Acoustics. 120: 949-957. DOI: 10.1115/1.2893925 |
0.42 |
|
| 1997 |
Denoyer KK, Peterson LD. Model Update Using Modal Contribution to Static Flexibility Error Aiaa Journal. 35: 1739-1745. DOI: 10.2514/2.43 |
0.376 |
|
| 1997 |
Doebling SW, Hemez FM, Peterson LD, Farhat C. Improved Damage Location Accuracy Using Strain Energy-Based Mode Selection Criteria Aiaa Journal. 35: 693-699. DOI: 10.2514/2.159 |
0.347 |
|
| 1997 |
Denoyer KK, Peterson LD. Method for Structural Model Update Using Dynamically Measured Static Flexibility Matrices Aiaa Journal. 35: 362-368. DOI: 10.2514/2.102 |
0.38 |
|
| 1996 |
Hinkle JD, Peterson LD, Doebling SW. Analysis of nonlinear mechanisms in a precision deployable structure using measured flexibility Journal of Spacecraft and Rockets. 33: 848-852. DOI: 10.2514/3.26848 |
0.458 |
|
| 1996 |
Doebling SW, Peterson LD, Alvin KF. Estimation of reciprocal residual flexibility from experimental modal data Aiaa Journal. 34: 1678-1685. DOI: 10.2514/3.13289 |
0.393 |
|
| 1996 |
Peterson LD. Bounding the Transient Response of Structures to Uncertain Disturbances Aiaa Journal. 34: 1245-1249. DOI: 10.2514/3.13219 |
0.36 |
|
| 1995 |
Alvin KF, Peterson LD, Park KC. Consistent model reduction of experimental modal parameters for reduced-order control Journal of Guidance Control and Dynamics. 18: 748-755. DOI: 10.2514/3.21456 |
0.356 |
|
| 1995 |
Layton JB, Peterson LD. Improved integrated structural control design using covariance control parameterization Aiaa Journal. 33: 1492-1495. DOI: 10.2514/3.12572 |
0.392 |
|
| 1995 |
Alvin KF, Peterson LD, Park KC. Minimal-order experimental component mode synthesis - New results and challenges Aiaa Journal. 33: 1477-1485. DOI: 10.2514/3.12570 |
0.32 |
|
| 1995 |
Alvin KF, Peterson LD, Park KC. Method for determining minimum-order mass and stiffness matrices from modal test data Aiaa Journal. 33: 128-135. DOI: 10.2514/3.12342 |
0.336 |
|
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