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DESCRIPTION: Developing optical payloads for aerospace applications requires multi-physics collaboration. This type of workflow involves designing an optical system and generating opto-mechanical behavior by realistically modelling the structural and thermal impacts experienced by a payload in-orbit.  \n \nThe Ansys software suite offers a streamlined optical simulation workflow that enables Structural-Thermal-Optical-Performance (STOP) analysis for aerospace applications. Interoperability between software packages eliminates time consuming tasks to interface simulation steps and allows for more time to be devoted to the engineering process. \n \nJoin us to learn how this workflow can be leveraged for a CubeSat operating in low Earth orbit. Beginning with an optical payload modelled using OpticStudio & OpticsBuilder, we will demonstrate how to perform finite difference and element analysis using Thermal Desktop & Ansys Mechanical. We will then showcase how to import the generated thermal and structural analysis data into the OpticStudio STAR module for STOP analysis.\n \nTo generate thermal loading data (e.g., solar flux) representative of in-orbit conditions, we will describe how Ansys Systems Tool Kit (STK) can be used to model the CubeSat orbit and interface with the STOP analysis workflow.  \n \nLearning Outcomes:  \n \n-   Understand how to bring a CubeSat optical payload through the stages of optical design, opto-mechanical design, and Structural-Thermal-Optical-Performance (STOP) analysis.\n-   Understand how Ansys Systems Tool Kit can be used to model the orbit of a satellite and determine the boundary conditions that can be used for thermal analysis.  \n-   Learn how to utilize Thermal Desktop & Ansys Mechanical to perform thermal and structural analyses for temperature distributions and optical surface deformations that will be experienced by the payload in low Earth orbit. \n-   Learn how to import temperature and deformation data into OpticStudio via the STAR Module to analyze the effects of the 	data on optical performance. \n
DTSTART:20230606T150000
DTEND:20230606T160000
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LOCATION:Online
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SUMMARY;LANGUAGE=es-es:Tecnowebinars.com - :: STOP Analysis: Simulating Realistic Optical Performance of a Low-Earth Orbit Satellite
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