Quadrotors' double-loop controller design with tensor product model transformation and partial fully actuated method

被引:1
作者
Chang, Fei [1 ,4 ]
Kang, Jia Pei [1 ]
Huang, Sha Ri Na [2 ]
Zhao, Guo Liang [1 ,3 ]
机构
[1] Inner Mongolia Univ, Coll Elect Informat Engn, Hohhot 010021, Peoples R China
[2] Inner Mongolia Agr Univ, Coll Sci, Hohhot 010018, Peoples R China
[3] Univ Alberta, Dept Elect & Comp Engn, Edmonton, AB T6R 2V4, Canada
[4] Inner Mongolia Power Grp Mengdian Informat & Telec, Hohhot 010020, Inner Mongolia, Peoples R China
基金
中国国家自然科学基金;
关键词
TP model transformation; Fully actuated control; Uniform design (UD) sampling; Hyper-grid sampling; Double loop control; AEROELASTIC WING SECTION; ATTITUDE-CONTROL; AIRCRAFT SUBJECT; STABILIZATION; SYSTEMS; ERROR;
D O I
10.1016/j.isatra.2024.05.023
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In the existing work of tensor product (TP) model transformation, the TP model transformation -based work on the quadrotor's control system design is scarce, the direct TP model transformation control strategy that applied to the quadrotor fails due to the calculation complexity, infeasibility of the huge amount of linear matrix inequalities, and the complexity of solving the linear matrix inequalities. To solve this problem, a partial TP model transformation -based double loop fuzzy controller has been studied in this work, the double -loop hybrid control scheme combines the fully actuated control method and the TP model transformation, while the fully actuated control method is used to the position subsystem control loop, and the TP model transformation based fuzzy controller is applied to the attitude control of the quadrotor. Moreover, for comparison purpose, a varying -input method based on TP model transformation is extended to the quadrotor's system control. The double -loop hybrid control scheme could also be extended with other TP model transformation based tensor sampling methods, such as, uniform sampling method and varying -input method. At last, the proposed algorithms are evaluated and compared on Parrot Mambo Minidrone, MFP450 and CUAV V5+ based hexarotor.
引用
收藏
页码:181 / 197
页数:17
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