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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:ZHANG Li-bin,CUI Nai-gang,PU Jia-lun.Research on nonlinear attitude control algorithm for upper stage during multi-satellite disposing[J].Journal of Harbin Institute Of Technology(New Series),2011,18(5):14-18.DOI:10.11916/j.issn.1005-9113.2011.05.003.
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Research on nonlinear attitude control algorithm for upper stage during multi-satellite disposing
Author NameAffiliation
ZHANG Li-bin School of Astronautics,Harbin Institute of Technology,Harbin 150001,China 
CUI Nai-gang School of Astronautics,Harbin Institute of Technology,Harbin 150001,China 
PU Jia-lun School of Astronautics,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
For the issues of attitude strong coupling and the increments of attitude errors of upper stage during multi-satellite disposing,a three-axis stability nonlinear attitude control algorithm via feedback linearization is presented.By the definitions of coordinates and the attitude angle during multi-satellite disposing,the attitude dynamics and kinematics equations with Euler angles described are built.And the equations are equivalently linearized based on feedback linearization theory.A three-axis nonlinear predictive control algorithm is designed and the system robustness is analyzed.An example of mathematical simulation is completed using the Matlab/Simulink environment.Simulation results showed that the control algorithm has good disturbance rejection,rapidity,stability and robustness.
Key words:  upper stage  attitude control  feedback linearization  nonlinear predictive control
DOI：10.11916/j.issn.1005-9113.2011.05.003
Clc Number:V448.22
Fund:

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