Ground Test and Numerical Simulation of Aerodynamic Interference of the Marsupial UAS

被引：5

作者：

Li, Huadong ^{[1
]}

Liu, Yiliang ^{[1
]}

Li, Daochun ^{[1
]}

Bie, Dawei ^{[1
]}

Kan, Zi ^{[1
]}

机构：

[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China

来源：

AEROSPACE | 2023年 / 10卷 / 02期

关键词：

marsupial UAS; momentum source method; aerodynamic interference; multiple drones; safe flight boundary; FLIGHT;

D O I：

10.3390/aerospace10020175

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The marsupial unmanned aircraft system (UAS) consists of a large parent unmanned aerial vehicle (UAV) and multiple small children UAVs that can be launched and recovered in the air. The employment of marsupial UAS can expand the mission range of small UAVs and enhance the collaborative capabilities of small UAVs. However, the serious aerodynamic interference between the parent UAV and the child UAV will affect the flight safety during the launch and recovery process. In this paper, the interference characteristics of marsupial UAS is investigated through ground tests and CFD simulation. Ground tests compared the lift and power of the child UAV with and without parent UAV interference in different areas, and the simulation extended the experimental scope. Three specific interference regions above the parent UAV are defined, including the area above the rotors, the area above body and the transition area. In the first two aeras, the variation of the disturbed lift is more than 30% of the child UAV weight. In the transition aera, the child UAV will be subjected to significant lift variations and asymmetric moments. According to the interference characteristics of different regions, the safe flight boundaries and the appropriate paths of children UAVs are proposed.

引用

页数：20