Within the scope of this project, a high-fidelity, six-degrees-of-freedom (6DOF) simulation model will be created to enable the detailed examination of the dynamic behavior of a designated fighter jet both on the ground and in the air. Prospective candidates will research open-source data to develop critical subsystem models of the aircraft, encompassing aerodynamics, propulsion, mass, and landing gear.

Subsequently, utilizing these models, custom controller and autopilot algorithms will be specifically designed for the aircraft. By the conclusion of the project, a visualization environment will be prepared wherein flight and ground scenarios can be visually analyzed, allowing all behaviors of the aircraft to be comprehensively verified through the simulation.

Criteria and Expectations

• The ability to effectively utilize MATLAB and/or Simulink software within system modeling processes.
• Demonstrated knowledge or experience in modeling aircraft dynamics or its sub-components (e.g., Aerodynamics, Propulsion, Landing Gear).
• High motivation for autopilot design and the development of control systems.
• The capability to generate effective solutions to engineering problems by utilizing open-source data, coupled with strong literature review skills.
• A strong interest in developing visualization environments for the detailed examination of simulation data.

Relevant Academic Departments

• Aeronautical Engineering
• Aerospace Engineering
• Control and Automation Engineering
• Mechatronics Engineering
• Mechanical Engineering