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6DOF Modelling of Quadcopter Including Wind Effects
Project type
Academic / Research
Date
May 2025
Location
Dallas, Texas
Role
Flight Dynamics & Simulation Engineer
Tools
MATLAB / Simulink
Scope
6DOF Multirotor Dynamics
Focus Area
Wind Disturbance Modeling & Algorithm Validation
Developed a high-fidelity 6 Degrees of Freedom (6DOF) simulation of a quadcopter in MATLAB/Simulink, capturing both translational and rotational dynamics under nominal and disturbed flight conditions. The model integrates aerodynamic forces, gravity, thrust vectoring, and gyroscopic effects, along with wind disturbance inputs for enhanced realism. This framework provides a robust environment for validating flight control algorithms and evaluating quadrotor stability under external perturbations.
