A constrained optimal PID-like controller design for spacecraft attitude stabilization

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A constrained optimal PID-like controller design for spacecraft attitude stabilization

In this paper, an optimal PID-like controller is proposed for a spacecraft attitude stabilization problem subject to continuous inequality constraints on the spacecraft angular velocity and control, as well as terminal constraints on the spacecraft attitude and angular velocity. The closed-loop stab...

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Bibliographic Details
Main Authors:	Li, C., Teo, Kok Lay, Li, Bin, Ma, G.
Format:	Journal Article
Published:	2012
Online Access:	http://hdl.handle.net/20.500.11937/24021

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