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Disturbance-observer-based formation-containment control for UAVs via distributed adaptive event -triggered mechanisms
Authors:Lili Wei  Mou Chen  Tao Li
Affiliation:1. NYUAD Research Institute, New York University Abu Dhabi, PO Box 129188, Abu Dhabi, United Arab Emirates;2. Engineering Division, New York University Abu Dhabi, Learning & Game Theory Laboratory (L&G-Lab), Saadiyat Campus PO Box 129188, United Arab Emirates;3. CONICET and Instituto Tecnológico de Buenos Aires, Av. Madero 399, Buenos Aires, Argentina;4. Instituto Argentino de Matemática - CONICET and Universidad de Buenos Aires, Paseo Colón 850, Buenos Aires, Argentina;5. Department of Automatic Control, Universitat Politècnica de Catalunya, Institut de Robòtica i Informàtica Industrial (CSIC-UPC), Llorens i Artigas, 4-6, 08028 Barcelona, Spain;6. School of Electrical and Electronic Engineering, Universidad de los Andes,Carrera 1A No 18A-10, Bogotá;1. State Key Laboratory of Reliability and Intelligence of Electrical Equipment, Hebei University of Technology, Tianjin, 300130, China;2. School of Artificial Intelligence, Hebei University of Technology, Tianjin, 300130, China;3. School of Electrical and Automation Engineering, Tianjin University, Tianjin, 300072, China
Abstract:In this paper, the adaptive event-triggered formation-containment control for unmanned aerial vehicles (UAVs) is investigated in the presence of multiple leaders and external disturbances. By utilizing the leader-following model, the reference leader provides the desired flight trajectory for multiple formation leaders while the followers are driven into the convex hull spanned by the formation leaders. Initially, some effective disturbance observers are designed to obtain the estimations for eliminating the negative effects of external disturbances. Secondly, in order to alleviate the network burden, a dynamic triggering law is designed for the adaptive event-triggered mechanism (AETM) and the triggering frequency is heavily related to the triggering errors. Then, by exploiting Kronecker product technique and Lyapunov stability theory, two sufficient conditions on the stability of closed-loop system are established, which can help achieve the desired formation control target. Furthermore, the controller gains and observer ones can be determined by calculating the derived linear matrix inequalities (LMIs). Finally, a simulation example is given to illustrate the feasibility of the designed control protocol.
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