Real-Time Attitude Stabilization of a Mini-UAV Quad-rotor Using Motor Speed Feedback

被引:22
|
作者
Gonzalez, Ivan [1 ,2 ]
Salazar, Sergio [3 ]
Torres, Jorge [1 ,2 ]
Lozano, Rogelio [3 ,4 ]
Romero, Hugo [3 ,5 ]
机构
[1] CINVESTAV IPN, Dept Automat Control, Mexico City 07360, DF, Mexico
[2] CINVESTAV IPN, UMI LAFMIA CNRS 3175, Mexico City 07360, DF, Mexico
[3] CINVESTAV IPN, UMI LAFMIA, Mexico City 07360, DF, Mexico
[4] Ctr Rech Royallieu, UTC HEUDIASyC, F-60205 Compiegne, France
[5] UAEH, ICBI AACyE, Mineral De La Reforma 42184, Hgo, Mexico
关键词
Quadrotor; Speed sensing feedback; Real-time; Embedded system; EMBEDDED CONTROL;
D O I
10.1007/s10846-012-9713-6
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
A real-time attitude stabilization control scheme is proposed for the efficient performance of a mini-UAV Quad-Rotor. Brushless DC (BLDC) motor speed sensing is performed by reflective sensors in order to obtain a robust stabilization of the vehicle in hovering mode both indoor and outdoor. The speed measurement has the advantage of introducing this state information directly in the closed loop control which should be very useful for achieving robust stabilization of the mini-UAV. Furthermore a stabilizing control strategy based on Control Lyapunov Function (CLF) is proposed. The control scheme contains two control loops. The inner loop is devoted to control the motors speed while the outer loop is devoted to control the attitude stabilization of a mini-UAV. Assuming that the motors can be considered as a disturbance of the system, then by the standard singular perturbation theory, we may conclude that the system is asymptotically stable. Finally, to verify the satisfactory performance of proposed embedded controller, simulations and experimental results of speed sensing feedback in BLDC motors of the Quad-rotor aircraft in the presence of disturbances are presented.
引用
收藏
页码:93 / 106
页数:14
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