Hovering Control of Flapping Wings in Tandem with Multi-Rotors

被引:1
|
作者
Dhole, Aniket [1 ]
Gupta, Bibek [1 ]
Salagame, Adarsh [1 ]
Niu, Xuejian [1 ]
Xu, Yizhe [1 ]
Venkatesh, Kaushik [1 ]
Ghanem, Paul [1 ]
Mandralis, Ioannis [2 ]
Sihite, Eric [2 ]
Ramezani, Alireza [1 ]
机构
[1] Northeastern Univ, Dept Elect & Comp Engn, Silicon Synapse Labs, Boston, MA 02115 USA
[2] CALTECH, Dept Aerosp Engn, Pasadena, CA USA
关键词
FLIGHT; DESIGN;
D O I
10.1109/IROS55552.2023.10341523
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
This work briefly covers our efforts to stabilize the flight dynamics of Northeatern's tailless bat-inspired micro aerial vehicle, Aerobat. Flapping robots are not new. A plethora of examples is mainly dominated by insect-style design paradigms that are passively stable. However, Aerobat, in addition for being tailless, possesses morphing wings that add to the inherent complexity of flight control. The robot can dynamically adjust its wing platform configurations during gaitcycles, increasing its efficiency and agility. We employ a guard design with manifold small thrusters to stabilize Aerobat's position and orientation in hovering, a flapping system in tandem with a multi-rotor. For flight control purposes, we take an approach based on assuming the guard cannot observe Aeroat's states. Then, we propose an observer to estimate the unknown states of the guard which are then used for closed-loop hovering control of the Guard-Aerobat platform.
引用
收藏
页码:6639 / 6644
页数:6
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