Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8055542 | Acta Astronautica | 2018 | 14 Pages |
Abstract
A case study was performed to find the best testing angles to match the acceleration responses of the centre of mass and sum of interface forces for all three axes, as well as the von Mises stress for an element by a fastening point. The angle optimisation method resulted in RMS values and PSD responses that were much closer to the coupled system when compared with traditional testing. The optimum testing configuration resulted in an overall average error significantly smaller than the traditional method. Crucially, this case study shows that the optimum test campaign could be a single equipment level test opposed to the traditional three orthogonal direction tests.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Charly Knight, Marcello Remedia, Guglielmo S. Aglietti, Guy Richardson,