Journal of Astronomy and Space Sciences

The Korean Space Science Society (한국우주과학회)
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ADAPTIVE BACKSTEPPING CONTROL FOR SATELLITE FORMATION FLYING WITH MASS UNCERTAINTY

  • Published : 2006.12.10
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Abstract

Satellite formation flying has become a critical issue in the aerospace engineering because it is considered as an enabling technology for many space missions. Thus, many nonlinear control theories have been developed for the tracking problem of satellite formation flying, which include full-nonlinear dynamics, external disturbances and parameter uncertainty. In this study, nonlinear adaptive control law is developed using an adaptive backstepping technique to solve the relative position tracking problem of the satellite formation flying in the presence of mass uncertainty and the bounded external disturbance. Simulation studies are included to demonstrate the proposed controller performance. The proposed controller is shown to guarantee the system stability against the external bounded disturbances in the presence of mass uncertainty.

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References

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Cited by

  1. Robust Satellite Formation Flying Through Online Trajectory Optimization using LQR and Neural Networks vol.47, pp.1, 2014, https://doi.org/10.3182/20140313-3-IN-3024.00173