Robot nonlinear control for Unmanned Aerial Vehicles' multitasking

被引:9
作者
Andaluz, Victor H. [1 ]
Gallardo, Cristian M. [1 ]
Chicaiza, Fernando A. [1 ]
Carvajal, Christian P. [1 ]
Morales, Jose [2 ]
Cuzco, Giovanny [3 ]
Morales, Vicente [4 ]
Vaca, Byron E. [2 ]
Samaniego, Nicolay [3 ]
机构
[1] Univ Fuerzas Armadas ESPE, Sangolqui, Ecuador
[2] Escuela Super Politecn Chimborazo, Riobamba, Ecuador
[3] Univ Nacl Chimborazo, Riobamba, Ecuador
[4] Univ Tecn Ambato, Ambato, Ecuador
关键词
Non-linear systems; Quadcopters; Stability and robustness proof; Unified motion control;
D O I
10.1108/AA-02-2018-036
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Purpose This paper aims to present a unified motion control scheme for quadcopters which not only solves the point stabilization and trajectory tracking problems but also the path following problem. Design/methodology/approach The control problem is solved based on the kinematic model of the unmanned aerial vehicles (UAV). Next, a dynamic compensation controller is considered through of a quadcopter-inner-loop system to independently track four velocity commands: forward, lateral, up/downward and heading rate. Stability and robustness of the whole control system are proved through the Lyapunov's method. To evaluate the controller's performance, a multi-user application which allows bilateral communication between a ground station and the Phantom 3 PRO quadrotor is developed. Findings The performance of the proposed unified controller is shown through real experiments for the different motion control objectives: point stabilization, trajectory tracking and path following. The experiments confirm the capability of the unified controller to solve different motion problems by an adequate selection of the control references. Originality/value This work proposes the design of three types of motion controllers, which can be switched to comply a task in outdoor. Based on the software development kit provided by the company DJI, an application to get and send data to the UAV is developed. By means of this application, the three tasks are tested and the robustness of the controllers is proved.
引用
收藏
页码:645 / 660
页数:16
相关论文
共 19 条
[1]  
Adamski M, 2016, J KONES POWERTRAIN T, V23, P11
[2]  
Ali Z.A., 2016, SENSORS, V16, P1
[3]  
Azari M.M., 2016, PROC IEEE GLOBECOM W, V2016, P1
[4]  
Bevan Elizabeth, 2015, Marine Turtle Newsletter, P19
[5]  
Biao Wang, 2010, 2010 IEEE Conference on Cybernetics and Intelligent Systems (CIS) and IEEE Conference on Robotics, Automation and Mechatronics (RAM 2010), P70, DOI 10.1109/ICCIS.2010.5518579
[6]  
Brandao A. S., 2011, 2011 9th IEEE International Conference on Control and Automation (ICCA 2011), P434, DOI 10.1109/ICCA.2011.6138018
[7]  
Brandao A.S., 2013, INT J ADV ROBOT SYST, V10, P1
[8]   Design and implementation of a robust and nonlinear flight control system for an unmanned helicopter [J].
Cai, Guowei ;
Chen, Ben M. ;
Dong, Xiangxu ;
Lee, Tong H. .
MECHATRONICS, 2011, 21 (05) :803-820
[9]   Control, navigation and collision avoidance for an unmanned aerial vehicle [J].
Chee, K. Y. ;
Zhong, Z. W. .
SENSORS AND ACTUATORS A-PHYSICAL, 2013, 190 :66-76
[10]  
Kaddouri Djamel M.A.A.B., 2016, MATH PROBL ENG, V2016, P1