Stochastic Launcher-Satellite Coupled Dynamic Analysis
Author:
Affiliation:
1. Institute of Engineering Mechanics, Leopold-Franzens University, 6020 Innsbruck, Austria
2. ESA, 2200 AG Noordwijk, The Netherlands
3. Andreas Kreis Consultancies, 7212 Seewis-Dorf, Switzerland
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.21154
Reference25 articles.
1. Uncertainty-based loads analysis for spacecraft: Finite element model validation and dynamic responses
2. Variational Coupled Loads Analyses: Reducing Risk in Development of Space-Flight Hardware
3. Simulation and the Monte Carlo Method
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