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		题名	作者	年代	出处	被引量
	1	Sensor Fault Estimation Filter Design for Discrete-time Linear Time-varying Systems显示文摘	WANG Zhen-Hua RODPIGUES Mickaelt THEILLIOL Didier SHEN Yi	2014	自动化学报2014，40，10：	9
	2	Flocking control of a fleet of unmanned aerial vehicles显示文摘	Adel BELKADI Zhixiang LIU Laurent CIARLETTA Youmin ZHANG Didier THEILLIOL	2018	Control Theory and Technology2018，16，2：	3
	3	Active model-based nonlinear system identification of quad tilt-rotor UAV with flight experiments显示文摘To propose an accurate and less complex model of a special unmanned aerial vehicle(UAV),namely tilt-rotor UAV(TRUAV), this study identifies the active model-based nonlinear system of a quadTRUAV. First, a nominal nonlinear model of the vehicle is formulated. Some unstructured nonlinearities are ignored to reduce the complexity of the model. Then, due to the unstable dynamics of the open-loop system,the format of this nominal model is considered to design an innovative smooth-switch attitude control via interconnection and damping assignment passivity-based control(IDA-PBC). Active model-based nonlinear system identification is studied for the vehicle with the designed control method and flight experiments.The model error vector is defined and estimated by the unscented Kalman filter(UKF) to improve the accuracy of the model. The main contribution of this paper is to identify the nominal nonlinear model and to develop an active model method of the quad-TRUAV. The attitude control method with an innovative smooth-switch structure is another contribution to flight experiments. Numerical results are displayed to present the experimental results and effectiveness of the proposed nonlinear models.	Zhong LIU Didier THEILLIOL Yuqing HE Feng GU Liying YANG Jianda HAN	2022	Science China(Information Sciences)2022，65，8：	1
	4	Event-triggered leader-following formation control for multi-agent systems under communication faults: application to a fleet of unmanned aerial vehicles显示文摘The main contribution of this paper is the design of an event-triggered formation control for leader-following consensus in second-order multi-agent systems(MASs)under communication faults.All the agents must follow the trajectories of a virtual leader despite communication faults considered as smooth time-varying delays dependent on the distance between the agents.Linear matrix inequalities(LMIs)-based conditions are obtained to synthesize a controller gain that guarantees stability of the synchronization error.Based on the closed-loop system,an event-triggered mechanism is designed to reduce the control law update and information exchange in order to reduce energy consumption.The proposed approach is implemented in a real platform of a fleet of unmanned aerial vehicles(UAVs)under communication faults.A comparison between a state-of-the-art technique and the proposed technique has been provided,demonstrating the performance improvement brought by the proposed approach.	VAZQUEZ TREJO Juan Antonio GUENARD Adrien ADAM-MEDINA Manuel PONSART Jean-Christophe CIARLETTA Laurent ROTONDO Damiano THEILLIOL Didier	2021	Journal of Systems Engineering and Electronics2021，32，5：	1
	5	Actuator Fault-tolerant Control Design:Demonstration on A Three-Tank System 显示文摘	NOURA Hassan THEILLIOL Didier SAUTER Dominique	2000	International Journal of Systems Science2000，31，9：	1

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