Quadrotor drone response data empty and with load

The data presented describe the flight response of quadrotor drone prototype to impulsive maneuver in the rolling axes, in the conditions empty and with load. The angular velocity of prototype is collected by a gyroscope, with data that describing the response of the system. The data have potential for mathematical modelling through the system identification, being base to determine flight control systems for drones and tuning control systems. The data reported in this paper refer to the impulsive response of a drone quadrotor in real conditions of flight, in the situations of empty and with load. Data consist of the angular velocity of drone, how response an impulsive maneuver in the rolling axis, for two configurations of the useful load. In first situation, the drone flies empty, while in the second situation, the drone flies with full useful load of 1000 grams. The data of both situations are presented in matrices, accompany this paper in Matlab format and labelled according to the configuration they are representative. As an example, the matrices are composed of two columns, the first column shows the sampling time and the second column presents angular velocity captured by the gyroscope coupled to the drone. The sampling time of the data is 0.005 seconds, being performed 80 samples.