[ designing geometry ]010%

[06] Project

Flexible Spacecraft Solar Panel Dynamics

MATLABFEAModal analysisDynamics

A coupled structural and dynamics model of flexible solar panels on a spacecraft, used to study how they bend and vibrate and how that affects the spacecraft.

Role
Robotics Engineering Intern, RADL
Year
2025
Model
Coupled FEA and dynamics
Studies
Deformation and vibration

Overview

Solar arrays are large and light, so they flex. When the spacecraft turns, the panels vibrate, and the vibration pushes back on the spacecraft. Treating them as rigid hides that.

How it works

The panels were modeled with finite elements to find how they bend and twist. Those shapes were reduced to a few modes and coupled to the spacecraft's motion, so each one affects the other.

Result

The coupled model gave better predictions of how the panels deform and respond than modeling them separately.