首页> 外文期刊>Journal of guidance, control, and dynamics >Rapid singularity-escape steering strategy for single-gimbal control moment gyroscopes
【24h】

Rapid singularity-escape steering strategy for single-gimbal control moment gyroscopes

机译:单控制力矩陀螺仪的快速奇异逸出转向策略

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

To enable the quickest possible escape from an impassable singular surface, a rapid singularity-escape steering strategy is proposed. This steering strategy works when encountering an impassable singular surface. This strategy consists of three main steps. The first step is to determine the nearest escapable point, which is always on the edge of the impassable singular surface. The second step is to calculate the torque direction that is required to ensure that the angular momentum rapidly moves toward the nearest escapable point. The third step is to apply a steering law designed to function even on a singular surface. In addition, the gimbal rates calculated using this steering law can produce a torque along the required torque direction with the maximum capability of the single-gimbal control moment gyroscope system to ensure rapid escape from the singular surface. For the proposed steering strategy, only a small amount of data must be stored in advance. Finally, two sets of simulations are presented to verify that this steering strategy can drive the angular momentum to rapidly escape from a singular surface.
机译:为了尽可能快地从不可逾越的奇异表面逸出,提出了一种快速的奇异逸出转向策略。当遇到不可逾越的奇异表面时,此转向策略将起作用。该策略包括三个主要步骤。第一步是确定最接近的可转义点,该点始终在不可逾越的奇异曲面的边缘上。第二步是计算所需的转矩方向,以确保角动量迅速移向最近的可逃逸点。第三步是应用设计成即使在奇异表面上也能起作用的转向定律。此外,使用此转向定律计算出的万向节速率可沿所需扭矩方向产生扭矩,同时具有单万向节控制力矩陀螺仪系统的最大能力,可确保从奇异表面快速逃逸。对于建议的转向策略,仅必须预先存储少量数据。最后,提出了两组模拟,以验证这种转向策略可以驱动角动量快速从奇异表面逃逸。

著录项

  • 来源
    《Journal of guidance, control, and dynamics》 |2017年第12期|3199-3210|共12页
  • 作者单位

    Harbin Institute of Technology, Research Center of Satellite Technology, Harbin, China;

    Harbin Institute of Technology, Research Center of Satellite Technology, Harbin, China;

    Harbin Institute of Technology, Research Center of Satellite Technology, Harbin, China;

    Polytechnic University of Milan, Department of Aerospace Science and Technology, Milan, Italy;

  • 收录信息
  • 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