This thesis explores the application of lattice optimization, through honeycomb and tetrahedral structures, to develop light yet resistant camera drone frames. Through the use of the structures for their strength-to-weight ratio and additively manufacturability, the project aims to improve drone performance in terms of flight duration, maneuverability, and stability of the camera. Through the use of topology optimization and structural simulation, the thesis evaluates how such lattice structures distribute loads, absorb impact, and resist vibration during flight. Using SolidWorks for 3D modeling and ANSYS for modeling, finite element analysis (FEA) and modal analysis, the study applies topology optimization techniques to strategically place material only where needed, enhancing the frame’s mechanical performance while minimizing mass. This thesis explores the application of lattice optimization—more specifically The honeycomb lattice, which has excellent in-plane stiffness and energy absorption, is applied to flat frame sections, while the tetrahedral lattice offers isotropic strength that is well suited for three-dimensional structure regions. The thesis concludes with design recommendations that unify both lattice types according to functional zones in the frame, and emphasizes the role of manufacturing constraints, material properties, and multi-objective optimization in bringing high-performance drone structures to fruition.