Experimental Study of Problem of Estrangement of AR. Drone Four Rotor Helicopter Velocity Parameter Calculated by the Internal IMU
Abstract
For four rotor helicopter system, the velocity parameter is important for stable real-time control, and the velocity is calculated by the IMU (Internal Measurement Unit) from the three-axis acceleration and gyro sensors.
Since the IMU unit developed and designed for multi-purpose use, high-frequency range of the acceleration/gyro sensors information was used for estimating the velocity and it is afraid to do overestimation of the velocity especially when the drone collision against the wall (even with a slight contact) and the impact due to blasts. The result shows that the IMU unit calculated velocity was divergent 20 times from the real velocity measured from the camera on the ceiling even when low speed contact with a wall (25 cm/sec speed). When the estimated velocity parameter would be used for the position control and stabilizing of AR. Drone helicopter, it will be necessary to consider the problem of the estrangement of the velocity to develop the drone system for inspection at infrastructure equipment such as the bridge or tunnel.
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Introduction
In this paper, the velocity parameter obtained from the IMU (Internal Measurement Unit) in AR. Drone four rotor helicopter 1.0 was measured and analyzed, and it was found that the velocity parameter was calculated as an estrangement fashion when the drone touch against a wall with a slight impact. The IMU is one of the standard equipment of the drone system, since the information of acceleration and gyro sensors is indispensable for real-time stable posture controlling [1-7]. In addition, the velocity parameter is also estimating at the same time in the IMU, and it was typically used for the "space position" controlling and stabilizing process for drone controlling [1,8-16]. Since the IMU is developed and designed for multi-purpose use, high-frequency range of the acceleration and gyro sensors information was used for estimating the velocity parameter and it is afraid to do overestimation of the velocity especially when the drone collides against object such as wall or tree branches (Fig.1).Also, impacts from wind flow blasts would be afraid to do overestimation of the velocity. The main object of this paper is to compare the real velocity value measured from the camera on the ceiling with the IMU output estimated velocity parameter in the 𝑥 − 𝑦space in the room (Fig.2) to confirm the effect of the overestimation of the velocity parameter by the IMU.
Conclusion
In this paper, the velocity parameter obtained from the IMU (Internal Measurement Unit) in AR. Drone four rotor helicopter 1.0 was measured and analyzed, and it was found that the velocity parameter was calculated as an overestimated fashion when the drone touch against the wall with a slight impact. For four rotors helicopter system, the velocity parameter is important for stable real-time control, and the velocity is generally calculated by the IMU (Internal Measurement Unit) from the three-axis acceleration and gyro sensors. The result shows that the IMU estimating velocity 𝑣𝑦 𝑒 was divergent 20 times from the real velocity 𝑣𝑦measured from the camera on the ceiling even when low speed contact with a wall (25 cm/sec speed). When the estimated velocity parameter would be used for the position control and stabilizing of AR. Drone helicopter, it will be necessary to consider the problem of the estrangement of the velocity to develop the drone system for inspection at infrastructure equipment such as the bridge or tunnel.