Adaptive Finite-time Orbit Control for Spacecraft Formation with External Disturbances
2022 41st Chinese Control Conference (CCC)(2022)
摘要
This paper addresses the finite-time orbit control problem for spacecraft formation flying with external disturbances. A new finite-time tracking control strategy with adaptation law and the adding one power integrator method 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 external disturbances. Finally, an example is shown to validate the effectiveness of the proposed finite-time tracking controller.
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关键词
Finte-time Control,Spacecraft Formation Flying,backstepping method
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