Skip to Main Content

From Concept to CubeSat: Mission-Level STOP Analysis Deep Dive

Part Two of The Ansys Optics Concept to CubeSat Webinar to Workshop Series

In this session we will build on the concepts introduced in the previous webinar to demonstrate a fully automated multiphysics mission-level STOP analysis using Ansys simulation software including Ansys Zemax OpticStudio STAR, Ansys STK, Ansys ModelCenter, Ansys Thermal Desktop and Ansys Mechanical. The audience will experience a software feature update, an extended live demonstration of a complete CubeSat application example from concept through performance validation, and exclusive insights from an aerospace industry innovator. Plus interactive Q&A, live polls, and networking opportunities to solve your toughest design challenges.

Date/Time:
August 27, 2026

Session 1: 9:00 am EDT
Session 2: 2:00 pm EDT

Venue:
Virtual

Session 1: 9:00 AM EDT

Register Now

Session 2: 2:00 PM EDT

Register Now

Overview

Building on the concepts introduced in our previous webinar (CubeSat Optical Systems: Design Theory and Multiphysics Workflow Introduction), this technical deep dive will demonstrate how an integrated multiphysics workflow can be used to design, analyze, and optimize CubeSat platforms with demanding optical payload requirements. As mission goals continue to push the limits of small satellite performance, understanding the interaction between thermal environments, structural dynamics, optical performance, and attitude control systems becomes essential for achieving mission success.

Through an extended live demonstration, attendees will follow a representative CubeSat optical payload from concept to performance assessment using Ansys Zemax OpticStudio, Ansys Mechanical, and STAR module. The session will show how environmental loads and spacecraft dynamics propagate through the system and ultimately impact image quality, pointing accuracy, and line-of-sight (LOS) stability. Special focus will be placed on identifying and quantifying the root causes of LOS jitter and optical performance degradation.

Participants will learn how to connect thermal, structural, and optical analyses within a unified digital engineering framework to evaluate design tradeoffs before hardware is built. The live workflow will illustrate how thermal gradients create optical misalignments, how structural vibrations affect pointing performance, and how these effects can be translated directly into system-level optical metrics. Practical modeling methods, best practices, and simulation strategies will be discussed throughout the session.

What Attendees Will Learn

  • Understand how an integrated multiphysics workflow can be used to design, analyze, and optimize CubeSat platforms with demanding optical payload requirements.
  • Evaluate the interactions between thermal environments, structural dynamics, optical performance, and attitude control systems and their impact on mission success.
  • Analyze how environmental loads and spacecraft dynamics affect image quality, pointing accuracy, and line-of-sight (LOS) stability.
  • Identify and quantify the root causes of LOS jitter and optical performance degradation in CubeSat optical systems.
  • Apply a unified digital engineering framework to connect thermal, structural, and optical analyses, evaluate design tradeoffs, and assess system-level optical performance before hardware is built.

Who Should Attend

  • Optical Engineers
  • Satellite System Engineers
  • Optomechanical Engineers
  • Photonics Engineers
  • Mechanical Engineers designing space-based optical systems
  • Aerospace Systems Engineers

Speaker

  • Mojtaba Falahati, Applications Engineering, Staff Engineer

Secure your spot!