(주)써모

Join us as we demonstrate how dynamic satellite simulation of high-fidelity orbiting objects can be performed with MuSES™, including thermal-electrical analysis and EO/IR sensor radiance prediction.

In this webinar, we outline:

·       The motivation for thermal, electrical and EO/IR satellite simulation

·       A brief review of orbital physics relevant to thermal simulation with MuSES™

·       A description of our transient simulation methodology for orbiting satellites

·       The incorporation of PV panels and multi-cell battery packs into coupled thermal-electric MuSES™ simulations

·       An approach to predicting battery lifetime and PV degradation during multi-year orbital missions

·       Thermal and EO/IR radiometric signature results for a communications satellite in both LEO and GEO scenarios

·       Sensitivity of radiometric EO/IR satellite signature to optical surface properties, operational state and other model parameters