Fuzzy Gain-Scheduling PID for UAV Position and Altitude Controllers

被引:21
|
作者
Melo, Aurelio G. [1 ]
Andrade, Fabio A. A. [2 ,3 ]
Guedes, Ihannah P. [4 ]
Carvalho, Guilherme F. [4 ]
Zachi, Alessandro R. L. [4 ]
Pinto, Milena F. [4 ]
机构
[1] Univ Fed Juiz de Fora, Dept Elect Engn, BR-36036900 Juiz De Fora, Brazil
[2] Univ South Eastern Norway USN, Fac Technol Nat Sci & Maritime Sci, Dept Microsyst, N-3184 Borre, Norway
[3] NORCE Norwegian Res Ctr, N-5838 Bergen, Norway
[4] Fed Ctr Technol Educ Rio de Janeiro, Dept Elect Engn, BR-20271110 Rio De Janeiro, Brazil
关键词
gain schedule technique; fuzzy-PID strategy; position controller; altitude controller; UAV; SLIDING MODE CONTROLLER; TRAJECTORY TRACKING; NEURAL-NETWORK; DESIGN;
D O I
10.3390/s22062173
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
Unmanned aerial vehicle (UAV) applications have evolved to a wide range of fields in the last decade. One of the main challenges in autonomous tasks is the UAV stability during maneuvers. Thus, attitude and position control play a crucial role in stabilizing the vehicle in the desired orientation and path. Many control techniques have been developed for this. However, proportional integral derivative (PID) controllers are often used due their structure and efficiency. Despite PID's good performance, different requirements may be present at different mission stages. The main contribution of this research work is the development of a novel strategy based on a fuzzy-gain scheduling mechanism to adjust the PID controller to stabilize both position and altitude. This control strategy must be effective, simple, and robust to uncertainties and external disturbances. The Robot Operating System (ROS) integrates the proposed system and the flight control unit. The obtained results showed that the proposed approach was successfully applied to the trajectory tracking and revealed a good performance compared to conventional PID and in the presence of noises. In the tests, the position controller was only affected when the altitude error was higher, with an error of 2% lower.
引用
收藏
页数:21
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