CONTENTS
Volume 5, Number 2, 2018
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Spacecraft vibration testing: Benefits and potential issues
Ali R. Kolaini, Walter Tsuha and Juan P. Fernandez
pages 165-175.
DOI: 10.12989/aas.2018.5.2.165
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Transient Testing from LV / SC coupled analysis by new shock synthesis
Alain Girard, Etienne Cavro and Paul-Eric Dupuis
pages 177-186.
DOI: 10.12989/aas.2018.5.2.177
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Sine sweep effect on specimen modal parameters characterization
Nicolas Roy, Maxime Violin and Etienne Cavro
pages 187-204.
DOI: 10.12989/aas.2018.5.2.187
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Modelling and simulation of a closed-loop electrodynamic shaker and test structure model for spacecraft vibration testing
Steffen Waimer, Simone Manzato, Bart Peeters, Mark Wagner and Patrick Guillaume
pages 205-223.
DOI: 10.12989/aas.2018.5.2.205
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Feasibility study of the beating cancellation during the satellite vibration test
Alain Bettacchioli
pages 225-237.
DOI: 10.12989/aas.2018.5.2.225
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Utilizing virtual vibration tests to optimize physical endurance tests
Frederic Kihm
pages 239-249.
DOI: 10.12989/aas.2018.5.2.239
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A virtual shaker testing experience: Modeling, computational methodology and preliminary results
Pietro Nali, Alain Bettacchioli, Guglielmo Landi and Marco Gnoffo
pages 251-258.
DOI: 10.12989/aas.2018.5.2.251
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Static and dynamic load superposition in spacecraft structural analysis
Xavier Vaquer-Araujo, Florian Schöttle, Andreas Kommer and Werner Konrad
pages 259-275.
DOI: 10.12989/aas.2018.5.2.259
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Comparison of mass operator methods considering test uncertainties
K. R. Olympio, F. Blender, M. Holz, A. Kommer and R. Vetter
pages 277-294.
DOI: 10.12989/aas.2018.5.2.277