...
首页> 外文期刊>Journal of Spacecraft and Rockets >Passivity-Based Adaptive Finite-Time Trajectory Tracking Control for Spacecraft Proximity Operations
【24h】

Passivity-Based Adaptive Finite-Time Trajectory Tracking Control for Spacecraft Proximity Operations

机译:基于被动性的航天器近程自适应有限时间轨迹跟踪控制

获取原文
获取原文并翻译 | 示例
           

摘要

A passivity-based robust adaptive finite-time trajectory tracking control strategy is developed for a pursuer spacecraft proximity to a cooperative target spacecraft in space. The relative position vector between the pursuer and the target is required to direct toward the docking port of the target while the attitude of the two bodies must be synchronized. With the effective reference trajectory, the finite-time control of relative translational and relative rotational motions is finished simultaneously by using a unified passivity-based adaptive control method. Finite-time stability of the closed-loop system for six degree-of-freedom relative motion is proved in spite of the unknown inertial parameters and external disturbances. Numerical simulations including six-degree-of-freedom rigid-body dynamics are performed to demonstrate the effectiveness of the proposed controller.
机译:研制了一种基于无源性的鲁棒自适应有限时间轨迹跟踪控制策略,用于跟踪航天器与合作目标航天器在空间中的接近性。要求追踪器和目标之间的相对位置矢量指向目标的对接端口,同时必须使两个物体的姿态同步。通过有效的参考轨迹,可以使用基于无源性的统一自适应控制方法同时完成相对平移和相对旋转运动的有限时间控制。尽管存在未知的惯性参数和外部干扰,但仍证明了六自由度相对运动的闭环系统的有限时间稳定性。进行了包括六自由度刚体动力学在内的数值模拟,以证明所提出控制器的有效性。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2016年第1期|46-56|共11页
  • 作者

    Sun Liang;

  • 作者单位

    Beijing Univ Aeronaut & Astronaut, Div Res 7, Sci & Technol Aircraft Control Lab, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号