共 49 条
Composite block backstepping trajectory tracking control for disturbed unmanned helicopters
被引:35
作者:
Wang, Xiangyu
[1
,2
]
Yu, Xin
[1
,2
]
Li, Shihua
[1
,2
]
Liu, Jiyu
[3
]
机构:
[1] Southeast Univ, Sch Automat, Nanjing 210096, Jiangsu, Peoples R China
[2] Minist Educ, Key Lab Measurement & Control Complex Syst Engn, Beijing, Peoples R China
[3] Facri, Aviat Key Lab Sci & Technol Aircraft Control, Xian 710065, Shaanxi, Peoples R China
基金:
中国国家自然科学基金;
关键词:
Unmanned helicopters;
Disturbances;
Trajectory tracking control;
Feedforward-feedback composite control;
Blocking backstepping control;
Generalized proportional integral observer;
OBSERVER-BASED CONTROL;
SLIDING-MODE CONTROL;
NONLINEAR-SYSTEMS;
REJECTION CONTROL;
DESIGN;
POSITION;
ROTORCRAFT;
D O I:
10.1016/j.ast.2018.12.019
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
In this paper, the position and yaw angle trajectory tracking control problem is studied for unmanned helicopters subject to both matched and mismatched disturbances. To achieve the trajectory tracking goal, a feedforward-feedback composite control scheme is proposed based on the combination of the generalized proportional integral observer and the block backstepping control techniques. The controller design process mainly consists of two stages. In the first stage, some generalized proportional integral observers are developed for the helicopter system to estimate the mismatched, matched disturbances and their (higher-order) derivatives. In the second stage, the composite controller is designed by integrating the block backstepping control method and the disturbance estimates together. The proposed composite scheme guarantees asymptotic tracking performances for the position and yaw angle of the helicopter to the desired trajectories even in the presence of fast time-varying disturbances. Numerical simulations demonstrate the effectiveness of the proposed composite control scheme. (C) 2018 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:386 / 398
页数:13
相关论文