Adaptive Nonlinear Hierarchical Control for a Rotorcraft Transporting a Cable-Suspended Payload

被引:40
作者
Liang, Xiao [1 ,2 ]
Fang, Yongchun [1 ]
Sun, Ning [1 ]
Lin, He [1 ]
Zhao, Xingang [2 ]
机构
[1] Nankai Univ, Tianjin Key Lab Intelligent Robot, Inst Robot & Automat Informat Syst, Tianjin 300350, Peoples R China
[2] Chinese Acad Sci, Shenyang Inst Automat, State Key Lab Robot, Shenyang 110016, Peoples R China
来源
IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS | 2021年 / 51卷 / 07期
基金
中国国家自然科学基金;
关键词
Hierarchical control; Lyapunov methods; nonlinear control; rotorcraft transportation systems; SLIDING MODE CONTROL; TRACKING CONTROL; QUADROTOR; CONSTRUCTION; HELICOPTERS; STABILITY; SYSTEMS; DESIGN; FLIGHT;
D O I
10.1109/TSMC.2019.2931812
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Rotorcrafts, with satisfactory maneuver performance and ability under complex terrains unreachable for ground robots, are playing important roles for goods transportation. In this article, we focus on the control of the cable-suspended transportation way due to its lower costs and more agility of the rotorcraft's rotational motion. Compared with traditional crane systems and single rotorcrafts without loads, the aerial transportation system presents "double" underactuated property, stronger system nonlinearity, and more complex dynamic coupling, which are huge challenges for control schemes design. Meanwhile, aerial transportation usually suffers from external disturbances and uncertainties presented with aerodynamic damping coefficients and rope length. Additionally, overshoots of the rotorcraft's position are potential threats for flight safety, especially in confined and complex environments. To address these problems, a novel adaptive control scheme is designed, which ensures effective rotorcraft positioning and payload swing suppression with restricted overshoot amplitudes. Asymptotic results are obtained with rigorous theoretical derivations provided by the Lyapunov-based stability analysis and LaSalle's invariance theorem. Real-time experiments are performed to validate the effectiveness of the proposed control scheme even in the presence of external disturbances. To the best of our knowledge, this is the first method designed for aerial transportation systems which achieves simultaneous rotorcraft positioning and swing suppression, together with insurance for overshoot restriction even in the presence of parametric uncertainties.
引用
收藏
页码:4171 / 4182
页数:12
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