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- W1496072727 abstract "The Lyapunov control law basing ellipse reference orbit is proposed, which is used to solving the control problem of the leader-follower satellite formation. An in-track direction drift transition formation is proposed for the leader-follower formation capture and reconfiguration. The Lyapunov control law is derived within the drift formation, and the system pole assignment is executed basing on the second-order system's optimal damping. The pulse-width modulation scheme is presented for the propulsion output modulation. The simulation shows that the drift formation and control law can be used for the leader-follower formation control under a large aberration. The research proposed in the paper can be good material and reference for the satellite formation engineering application." @default.
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- W1496072727 date "2011-07-22" @default.
- W1496072727 modified "2023-09-23" @default.
- W1496072727 title "Lyapunov control for the leader-follower satellite formation" @default.
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