Satellite Analysis and Design

Research Project

The parametric design and optimization of the satellite composite laminated plates with conventional stacking sequence under static load. We create finite element code using MATLAB software to calculate the deformation of the composite satellite plate. The model has been created to study the effect of changing fiber orientation on the displacement of the composite satellite plate. The MATLAB code validates with ANSYS software.



  • Analysis and design of composite satellite structure
  • Design optimization using proper software (Using MATLAB)