Solar array deployment simulation using ADAMS software

Details Solar array deployment simulation using ADAMS software Solar array deployment simulation using ADAMS software

Dec 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985esasp.231...41r&link_type=abstract

In ESA Second European Space Mechanisms and Tribology Symposium p 41-46 (SEE N86-27353 18-18)

Computer Science

Deployment, Digital Simulation, Dynamic Structural Analysis, Solar Arrays, Spacecraft Structures, Computer Systems Programs, Design Analysis, Mechanical Drives, Prediction Analysis Techniques, Spacecraft Power Supplies

Scientific paper

The use of ADAMS program to predict dynamic phenomena during deployment of satellite solar arrays is reviewed. The program increases understanding of influences of constituent flexibility during deployment. The program contributes to optimization of the mechanism as to mechanical strength under deployment loads and latching shocks; motorization factor; and layout on the solar array. Prediction of all in orbit deployment cases (including possible failure cases) in order to be sure that no unexpected phenomenon perturb the space flight is also improved. The improved accuracy using ADAMS is verified by test prediction correlation.

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