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    华冰

    • 副研究员
    • 招生学科专业:
      光学工程 -- 【招收硕士研究生】 -- 航天学院
      控制科学与工程 -- 【招收硕士研究生】 -- 航天学院
      航空宇航科学与技术 -- 【招收硕士研究生】 -- 航天学院
      电子信息 -- 【招收硕士研究生】 -- 航天学院
    • 学历:南京航空航天大学
    • 学位:工学博士学位
    • 所在单位:航天学院
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    A study of PID and L1 adaptive control for automatic balancing of a spacecraft three-axis simulator

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    所属单位:航天学院

    发表刊物:Int. J. Intell. Comp. Cybern.

    摘要:Purpose: The three-axis simulator relies on the air film between the air bearing and the bearing seat to achieve weightlessness and the frictionless motion condition, which is essential for simulating the micro-disturbance torque of a satellite in outer space. However, at the beginning of the experiment, the disturbance torque caused by the misalignment between the center of gravity of the simulator and the center of rotation of the bearing is the most important factor restricting the use of the space three-axis simulator. In order to solve this problem, it is necessary to set the balance adjustment system on the simulator to compensate the disturbance torque caused by the eccentricity. The paper aims to discuss these issues. Design/methodology/approach: In this paper, a study of L1 adaptive automatic balancing control method for micro satellite with motor without other actuators is proposed. L1 adaptive control algorithm adds the low-pass filter to the control law, which in a certain sense to reduce the high-frequency signal and speed up the response time of the controlled system. At the same time, by estimating the adaptive parameter uncertainty in object, the output error of the state predictor and the controlled object can be stabilized under Lyapunov condition, and the robustness of the system is also improved. The automatic balancing method of PID is also studied in this paper. Findings: Through this automatic balancing mechanism, the gravity disturbance torque can be effectively reduced down to 10−6Nm, and the automatic balancing time can be controlled within 7 s. Originality/value: This paper introduces an automatic balancing mechanism. The experimental results show that the mechanism can greatly improve the convergence speed while guaranteeing the control accuracy, and ensuring the feasibility of the large angle maneuver of spacecraft three-axis simulator. © 2018, Emerald Publishing Limited.

    ISSN号:1756-378X

    是否译文:

    发表时间:2018-01-01

    合写作者:陈林,吴云华,陈志明

    通讯作者:华冰