2018 · 12 citations · 7 references
EngineeringAerospace EngineeringRobotics EngineeringAerial RoboticsFlight DynamicsUnmanned Aircraft SystemsAircraft ControlAircraft StabilityAttitude ControlController DesignFlight SimulationQuadrotor DynamicsAttitude DynamicsEuler-lagrange EquationsEuler-lagrange ModelingFlight Control ArchitectureFlight Dynamics ModelingFlight Mechanics ModelingPid Control DesignUnmanned Aerial Vehicle Control
In this paper mathematical model of quadrotor Unmanned Aerial Vehicle UAV was developed using Euler-Lagrange approach, then model parameters was identified using calculations and experimental tests. In order to validate the estimated model a PID controller for attitude stabilisation was designed and tested by several simulation and experimental step responses. Finally a flight test was successfully accomplished providing the adequacy of the model.
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