Vision-Based Safety-Critical Landing Control of Quadrotors With External Uncertainties and Collision Avoidance

被引:0
|
作者
Lin, Jie [1 ,2 ]
Miao, Zhiqiang [1 ,2 ]
Wang, Yaonan [1 ,2 ]
Wang, Hesheng [3 ,4 ,5 ]
Wang, Xiangke [6 ]
Fierro, Rafael [7 ]
机构
[1] Hunan Univ, Coll Elect & Informat Engn, Changsha 410082, Peoples R China
[2] Natl Engn Lab Robot Visual Percept & Control, Changsha 410073, Peoples R China
[3] Shanghai Jiao Tong Univ, Dept Automat, Key Lab Syst Control & Informat Proc, Shanghai 200240, Peoples R China
[4] Shanghai Jiao Tong Univ, Key Lab Syst Control & Informat Proc, Minist Educ China, Shanghai 200240, Peoples R China
[5] Harbin Inst Technol, State Key Lab Robot & Syst, Harbin 150001, Peoples R China
[6] Natl Univ Def Technol, Coll Intelligence Sci & Technol, Changsha 410073, Peoples R China
[7] Univ New Mexico, Dept Elect & Comp Engn, MARHES Lab, Albuquerque, NM 87131 USA
关键词
Collision avoidance; disturbance rejection; land-ing control; position-based visual servoing (PBVS); quadrotor; CONTROL BARRIER FUNCTIONS; TRACKING;
D O I
10.1109/TCST.2024.3363372
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 article addresses the quadrotors' safety-critical landing control problem with external uncertainties and collision avoidance. A geometrically robust hierarchical control strategy is proposed for an underactuated quadrotor, which consists of a slow outer loop controlling the position and a fast inner loop regulating the attitude. First, an estimation error quantified (EEQ) observer is developed to identify and compensate for the target's linear acceleration and the translational disturbances, whose estimation error has a nonnegative upper bound. Furthermore, an outer-loop controller is designed by embedding the EEQ observer and control barrier functions (CBFs), in which the negative effects of external uncertainties, collision avoidance, and input saturation are thoroughly considered and effectively attenuated. For the inner-loop subsystem, a geometric controller with a robust integral of the sign of the error (RISE) control structure is developed to achieve disturbances rejection and asymptotic attitude tracking. Based on Lyapunov techniques and the theory of cascade systems, it is rigorously proven that the closed-loop system is uniformly ultimately bounded. Finally, the effectiveness of the proposed control strategy is demonstrated through numerical simulations and hardware experiments.
引用
收藏
页码:1310 / 1322
页数:13
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