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• W4229446108 abstract "This work addresses the finite-time orbit control problem for spacecraft formation flying with external disturbances and limited data communication. A hysteretic quantizer is employed for data quantization in the controller-actuator channel to decrease the communication rate and prevent the chattering phenomenon caused by the logarithmic quantizer. Combined with the adding one power integrator method and backstepping technique, a new finite-time tracking control strategy with adaptation law is designed to ensure that the closed-loop system is practical finite-time stable, and that the tracking errors of relative position and velocity are bounded within finite-time despite with limited data communication and external disturbances. Finally, an example is shown to validate the effectiveness of the proposed finite-time tracking controller." @default.
• W4229446108 created "2022-05-11" @default.
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• W4229446108 date "2022-05-09" @default.
• W4229446108 modified "2023-09-25" @default.
• W4229446108 title "Finite-Time Orbit Control for Spacecraft Formation with External Disturbances and Limited Data Communication" @default.
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• W4229446108 doi "https://doi.org/10.1155/2022/1911820" @default.
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