Modelling and Simulation of Quadrotor Using Model-Based Design
DOI:
https://doi.org/10.54097/hset.v9i.1730Keywords:
model-based design, modelling, simulation, quadrotor.Abstract
In the recent years, the control of Unmanned Aerial Vehicles (UAV) has become one of the most interesting fields of research, especially for quadrotor aircraft due to the simple structure, superior maneuverability and low cost. This paper presents a Model-Based approach to develop the mathematical model of quadrotor and establish a control method to meet the target of the actual flight. It employs Simulink to design the Proportional Integral Derivative (PID) controller for altitude and attitude loop of quadrotor, and uses Stateflow to implement control logic method for different flight conditions and states.
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