M
Mengyin Fu
Researcher at Nanjing University of Science and Technology
Publications - 261
Citations - 7989
Mengyin Fu is an academic researcher from Nanjing University of Science and Technology. The author has contributed to research in topics: Kalman filter & Inertial navigation system. The author has an hindex of 41, co-authored 238 publications receiving 6284 citations. Previous affiliations of Mengyin Fu include Nanjing Institute of Technology & Beijing Institute of Technology.
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Consensus of Multi-Agent Systems With General Linear and Lipschitz Nonlinear Dynamics Using Distributed Adaptive Protocols
TL;DR: This technical brief considers the distributed consensus problems for multi-agent systems with general linear and Lipschitz nonlinear dynamics and finds that the adaptive consensus protocols here can be implemented by each agent in a fully distributed fashion without using any global information.
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Attitude stabilization of rigid spacecraft with finite‐time convergence
TL;DR: In this article, two sliding mode controllers are proposed to force the state variables of the closed-loop system to converge to the origin in finite time, and the second control design consists of the estimation of the uncertainty and disturbance by adaptive method and thus it achieves the decrease of undesired chattering effectively.
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Distributed containment control of multi‐agent systems with general linear dynamics in the presence of multiple leaders
TL;DR: In this article, a distributed dynamic containment controller based on the relative outputs of neighboring agents is constructed for both continuous-time and discrete-time cases, under which the states of the followers will asymptotically converge to the convex hull formed by those of the leaders if, for each follower, there exists at least one leader that has a directed path to that follower.
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Attitude Tracking of Rigid Spacecraft With Bounded Disturbances
TL;DR: The problem of attitude control for a spacecraft model that is nonlinear in dynamics with inertia uncertainty and external disturbance has been investigated and Adaptive law and extended state observer are applied.
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Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation
TL;DR: No prior knowledge of inertia moment is required for both of the proposed adaptive control laws, which implies that the designed control schemes can be applied in spacecraft systems with a large parametric uncertainty existing in inertial matrix or even in unknown inertial Matrix.