– Calibration and 6-DOF test of a unique inertial measurement unit (IMU) using a Quadrotor aircraft. The purpose of this paper is to discuss the above issue.
– An IMU with the special capability of measuring the angular acceleration was developed and tested. A Quadrotor aircraft is used as 6-DOF test platform. Kinematics modeling of the Quadrotor was used in the determination of the Euler angles, while Dynamics modeling aided in the design the closed loop controller. For safety, the flight test was performed on a 6-DOF constrained reduced-gravity test stand.
– The developed IMU is suitable for measuring states and its time derivatives of mini UAVs. Not only that but also a simple control algorithm can be integrated in the same processing unit (a 32 microcontroller in this case).
– The tested IMU as well as the safety constrained test techniques are unique.
Verification of a special inertial measurement unit using a Quadrotor aircraft
International Journal of Intelligent Unmanned Systems ; 2 , 1 ; 40-55
04.02.2014
16 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Test of a Special Inertial Measurement Unit using a Quadrotor Aircraft
British Library Conference Proceedings | 2012
|A Low Cost Inertial Measurement Unit for Business Aircraft
SAE Technical Papers | 1969
|Method for operating inertial measurement unit, inertial measurement unit and vehicle
Europäisches Patentamt | 2024
|