TY - JOUR
T1 - A Smooth Distributed Formation Control Method for Quadrotor UAVs under Event-Triggering Mechanism and Switching Topologies
AU - Huang, Yi
AU - Xu, Xiangfan
AU - Meng, Ziyang
AU - Sun, Jian
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - This paper focuses on the formation control problem of a team of quadrotor unmanned aerial vehicles (UAVs) subject to switching directed topologies. We present a distributed event-triggered formation control algorithm via hierarchical framework, which achieves the formation control objective with weak assumptions on switching topologies. In particular, we develop a distributed control force that enables the achievement of the target formation, which only relies on the neighbors' position information under event-triggering mechanism. The proposed algorithm can maintain smooth characteristics when confronted with discontinuities stemming from event-triggering mechanism and switching interactions among agents. Additionally, the boundedness of the command control force can be guaranteed by employing an auxiliary system. Subsequently, we develop an attitude tracking control algorithm to guarantee that the attitude error almost globally exponentially converges to zero. Finally, a numerical example is carried out to validate the theoretical results.
AB - This paper focuses on the formation control problem of a team of quadrotor unmanned aerial vehicles (UAVs) subject to switching directed topologies. We present a distributed event-triggered formation control algorithm via hierarchical framework, which achieves the formation control objective with weak assumptions on switching topologies. In particular, we develop a distributed control force that enables the achievement of the target formation, which only relies on the neighbors' position information under event-triggering mechanism. The proposed algorithm can maintain smooth characteristics when confronted with discontinuities stemming from event-triggering mechanism and switching interactions among agents. Additionally, the boundedness of the command control force can be guaranteed by employing an auxiliary system. Subsequently, we develop an attitude tracking control algorithm to guarantee that the attitude error almost globally exponentially converges to zero. Finally, a numerical example is carried out to validate the theoretical results.
KW - event-triggering mechanism
KW - Formation control
KW - switching topologies
KW - unmanned aerial vehicles (UAVs)
UR - http://www.scopus.com/inward/record.url?scp=85218970400&partnerID=8YFLogxK
U2 - 10.1109/TVT.2025.3545932
DO - 10.1109/TVT.2025.3545932
M3 - Article
AN - SCOPUS:85218970400
SN - 0018-9545
JO - IEEE Transactions on Vehicular Technology
JF - IEEE Transactions on Vehicular Technology
ER -