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Satellite formation flying with input saturation: An LMI approach | IEEE Conference Publication | IEEE Xplore

Satellite formation flying with input saturation: An LMI approach


Abstract:

In this paper, we consider a relative position control problem for a satellite formation flying system in a noncoplarnar and elliptical orbit. It is assumed that the angu...Show More

Abstract:

In this paper, we consider a relative position control problem for a satellite formation flying system in a noncoplarnar and elliptical orbit. It is assumed that the angular rate and angular acceleration are not known, but they are bounded. The system dynamics is designed with the bounded uncertain parameters. In the presence of input saturation, we develop a state feedback controller that guarantees stability of the system. Linear matrix inequality (LMI) conditions are proposed to design the feedback controller. Finally, numerical simulation is presented to demonstrate the validity of the proposed controller.
Date of Conference: 28-30 September 2011
Date Added to IEEE Xplore: 17 October 2011
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Conference Location: Denver, CO, USA

References

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