Modeling and Attitude Control of a Spinning Spacecraft with Internal Moving Mass

Peng Fei Guo; Liang Yu Zhao

doi:10.4028/www.scientific.net/AMR.760-762.1216

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 760-762Modeling and Attitude Control of a Spinning...

Modeling and Attitude Control of a Spinning Spacecraft with Internal Moving Mass

Abstract:

An attitude control system of a spinning spacecraft with internal moving mass is presented in this paper. This system consists of a rigid body and two internal radial moving masses. The mathematical model, including attitude kinematics and nonlinear dynamics equations, is established based on Newtonian mechanics. The control law is designed based on the linear-quadratic-regulator (LQR) theory. The performance of the controller is demonstrated in numerical simulation, and the response shows that the attitude control system is stable and effective.

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Periodical:

Advanced Materials Research (Volumes 760-762)

Pages:

1216-1220

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.760-762.1216

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Online since:

September 2013

Authors:

Peng Fei Guo, Liang Yu Zhao

Keywords:

Attitude Control, LQR, Moving Mass, Spinning Spacecraft

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