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Composite control method for stabilizing spacecraft attitude in terms of Rodrigues parameters 被引量:8

Composite control method for stabilizing spacecraft attitude in terms of Rodrigues parameters
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摘要 In this paper, the attitude stabilization problem of a rigid spacecraft described by Rodrigues parameters is investigated via a composite control strategy, which combines a feedback control law designed by a finite time control technique with a feedforward compensator based on a linear disturbance observer (DOB) method. By choosing a suitable coordinate transformation, the spacecraft dynamics can be divided into three second-order subsystems. Each subsystem includes a certain part and an uncertain part. By using the finite time control technique, a continuous finite time controller is designed for the certain part. The uncertain part is considered to be a lumped disturbance, which is estimated by a DOB, and a corresponding feedforward design is then implemented to compensate the disturbance. Simulation results are employed to confirm the effectiveness of the proposed approach. In this paper, the attitude stabilization problem of a rigid spacecraft described by Rodrigues parameters is investigated via a composite control strategy, which combines a feedback control law designed by a finite time control technique with a feedforward compensator based on a linear disturbance observer (DOB) method. By choosing a suitable coordinate transformation, the spacecraft dynamics can be divided into three second-order subsystems. Each subsystem includes a certain part and an uncertain part. By using the finite time control technique, a continuous finite time controller is designed for the certain part. The uncertain part is considered to be a lumped disturbance, which is estimated by a DOB, and a corresponding feedforward design is then implemented to compensate the disturbance. Simulation results are employed to confirm the effectiveness of the proposed approach.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2013年第3期687-696,共10页 中国航空学报(英文版)
基金 Natural Science Foundation of China(61074013,61203011) Specialized Research Fundfor the Doctoral Program of Higher Education of China(20090092110022) New Century Excellent Talents in University(NCET-10-0328) the Scientific Research Foundation of Graduate School of Southeast University
关键词 Attitude control Composite control Disturbance observer Finite time control law SPACECRAFT Attitude control Composite control Disturbance observer Finite time control law Spacecraft
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