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6DOF Modelling of a rocket with guidance and controller
Date
March 2024
Location
Dallas, Texas
Project type
Simulation / Flight Systems / Control Engineering
Tools
MATLAB / Simulink
Scope
3DOF & 6DOF Modeling
Focus Area
Missile Guidance & Environmental Robustness
Developed a high-fidelity simulation of a ballistic missile system using aerodynamic and environmental data in Simulink. The project incorporated both 3DOF and 6DOF models to analyze flight dynamics, stability, and trajectory response under realistic operational conditions, including wind gusts and lateral crosswinds.
Multiple guidance laws were designed and tested to enhance terminal accuracy in the presence of dynamic disturbances. Each controller was evaluated for robustness, responsiveness, and adaptability—ensuring reliable performance across mission profiles.
