| Citation: | MA Mingyu, DONG Chaoyang, WANG Qing, et al. Cooperative attitude control on SO(3) for multiple spacecraft with time-varying gain ESO[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(9): 1797-1807. doi: 10.13700/j.bh.1001-5965.2017.0719(in Chinese)
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This paper is concerned with the cooperative attitude control of multiple spacecraft, and the control design method on special orthogonal group (SO(3)) with disturbance is studied. The multiple spacecraft system is modeled using SO(3) method and directed communication topology. Then, a time-varying gain extended state observer (ESO) is proposed to estimate the total disturbance in the system, and it lessens the peaking phenomenon. The control commands are formulated in the form of rotation matrices using the information of adjacent spacecraft. Thus, the cooperative controller based on SO(3) method is designed, and at the same time ESO output is used to compensate the disturbance on the system. The convergence of the ESO and the stability of the closed-loop system are analyzed in this paper, which shows that the attitudes of the multiple spacecraft could reach stable consensus. Simulation is conducted to verify the effectiveness of the proposed method.
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