Altitude and Attitude Quadrotor Control based on Adaptive Sliding Mode Controller with Input Saturation

被引:2
|
作者
Brahim, Khelil Sidi [1 ,2 ]
Terki, Nadjiba [3 ]
El Hajjaji, Ahmed [4 ]
Lara, David [5 ,6 ]
机构
[1] Univ Biskra, Dept Elect Engn, LMSE Lab, Biskra, Algeria
[2] Univ Picardie Jules Verne UPJV, MIS Lab, Amiens, France
[3] Univ Biskra, Dept Elect Engn, LESIA Lab, Biskra, Algeria
[4] UPJV, MIS Lab, Amiens, France
[5] CONACYT, Mexico City, DF, Mexico
[6] TECNM Misantla, Misantla, Mexico
关键词
TRACKING CONTROL;
D O I
10.1109/MED54222.2022.9837256
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper deals with the adaptive robust tracking control problem of a quadrotor under parametric uncertainties, actuator saturation and external wind disturbances. An adaptive robust control strategy is proposed to deal with this tracking problem. To solve the actuator saturation problem, an auxiliary system with adaptation law is considered. Global stability of the resulting closed loop system is analyzed using the sliding mode approach and the lyapunov theory. The proposed control strategy is developed to control the altitude system and attitude system representing the rotation angles in the presence of external perturbations, uncertainties and input saturation. The proposed control scheme is finally verified through various tests of simulation, also an experimental validation is carried on Parrot Mambo minidrone proving its effectiveness.
引用
收藏
页码:456 / 461
页数:6
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