Unified Motion Control for Multilift Unmanned Rotorcraft Systems in Forward Flight

被引:1
|
作者
Salinas, Lucio R. R. [1 ,2 ]
Gimenez, Javier [3 ]
Gandolfo, Daniel C. C. [3 ]
Rosales, Claudio D. D. [3 ]
Carelli, Ricardo [3 ]
机构
[1] Univ Bristol, Dept Engn Math, Bristol BS8 1TH, England
[2] Univ Bristol, Bristol Robot Lab, Bristol BS8 1TH, England
[3] Univ Nacl San Juan UNSJ, Natl Sci & Tech Res Council CONICET, Inst Automat INAUT, San Juan, Argentina
关键词
Forward flight; load equalization; multilift; unified motion control; unmanned aerial vehicles (UAVs); AERIAL VEHICLES UAVS; CIVIL APPLICATIONS; SUSPENDED-LOAD; TRANSPORTATION; MANIPULATION; OPTIMIZATION; HELICOPTER; DRONES;
D O I
10.1109/TCST.2023.3240541
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Interest in multilift rotorcraft systems has reemerged in recent years to overcome some of the problems in single unmanned aerial vehicle handling and delivery systems. Using multiple unmanned rotorcrafts (URs), the load weight can be evenly distributed among the vehicles, extending the flight time and therefore increasing the working distance of such systems. Moreover, with a slung-load configuration, bigger size packages with complex shape and equipment that may interfere with the onboard electronics can be carried. In this context, this article presents a payload-based unified motion control that allows any number of URs to cooperatively transport a slung load in forward flight. The motion control comprises path-following and trajectory-tracking algorithms, considers obstacle avoidance, implements a specific strategy for load weight distribution (load equalization) by regulating the relative altitude of each UR, and is robust to disturbances such as wind. In addition, this work shows that load equalization is essential for slung-load cooperative transport, especially in forward flight. The controller's stability is analytically studied and the good performance of the system is demonstrated through exhaustive simulations using validated dynamic models for mini-helicopters, cables, and payload. Finally, the relation between load weight and number of URs is analyzed by considering several scenarios.
引用
收藏
页码:1607 / 1621
页数:15
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