TY - GEN
T1 - Event-Triggered Attitude Controller Design for Unmanned Aerial Vehicles under Cyber Attacks
AU - Han, Seungyong
AU - Guo, Xuyang
AU - Jin, Yongsik
AU - Lim, Yongseob
AU - Kommuri, Suneel Kumar
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - This paper proposes an event-triggered attitude controller design method for unmanned aerial vehicles (UAVs) under cyber attacks. Versatile UAVs are capable of transmitting the measurement or receiving control signals through network channels. In the controller design for such UAVs, it is required to consider two distinctive features. The first one is that the strategy of updating the control signal is important for saving the limited energy consumption. The other one is that the UAVs are vulnerably exposed to threats of malicious attacks through network channels. For enhanced energy efficiency and improved stability, the event-triggered mechanism (ETM) and the attitude controller are simultaneously designed. By utilizing Lyapunov- Krasovskii functionals (LKFs), the sufficient conditions for the co-design are derived in terms of linear matrix inequalities (LMIs). For a 3-degrees of freedom (DOF) quadcopter system, the simulation results are presented to validate the proposed attitude control method.
AB - This paper proposes an event-triggered attitude controller design method for unmanned aerial vehicles (UAVs) under cyber attacks. Versatile UAVs are capable of transmitting the measurement or receiving control signals through network channels. In the controller design for such UAVs, it is required to consider two distinctive features. The first one is that the strategy of updating the control signal is important for saving the limited energy consumption. The other one is that the UAVs are vulnerably exposed to threats of malicious attacks through network channels. For enhanced energy efficiency and improved stability, the event-triggered mechanism (ETM) and the attitude controller are simultaneously designed. By utilizing Lyapunov- Krasovskii functionals (LKFs), the sufficient conditions for the co-design are derived in terms of linear matrix inequalities (LMIs). For a 3-degrees of freedom (DOF) quadcopter system, the simulation results are presented to validate the proposed attitude control method.
KW - Event-triggered mechanism
KW - Lyapunov-Krasovskii functionals
KW - attitude controller
KW - false-data injection attacks
UR - http://www.scopus.com/inward/record.url?scp=85199600858&partnerID=8YFLogxK
U2 - 10.1109/ISIE54533.2024.10595751
DO - 10.1109/ISIE54533.2024.10595751
M3 - Conference Proceeding
AN - SCOPUS:85199600858
T3 - IEEE International Symposium on Industrial Electronics
BT - 2024 33rd International Symposium on Industrial Electronics, ISIE 2024 - Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 33rd International Symposium on Industrial Electronics, ISIE 2024
Y2 - 18 June 2024 through 21 June 2024
ER -
