Research on nonlinear attitude control algorithm for upper stage during multi-satellite disposing
ZHANG Li-bin, CUI Nai-gang, 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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Research on nonlinear attitude control algorithm for upper stage during multi-satellite disposing
本站小编 哈尔滨工业大学/2019-10-23
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