首页> 外文会议>AAS/AIAA Spaceflight Mechanics Meeting >AUTONOMOUS SPACECRAFT ATTITUDE RESOURCE SHARING
【24h】

AUTONOMOUS SPACECRAFT ATTITUDE RESOURCE SHARING

机译:自主航天器态度资源共享

获取原文

摘要

This paper investigates the use of relative attitude sharing between two spacecraft. The first, sharing, spacecraft, has an inertial attitude sensor. The second, receiving, spacecraft lacks an attitude sensor. The sharing spacecraft is able to sense relative attitude, enabling determination of the inertial attitude of the receiving spacecraft composed with the inertial attitude of the sharing spacecraft. Relative attitude is assumed to be available only under certain alignment conditions consistent with proper orientation of a passive relative attitude sensor on the sharing spacecraft and attitude fiducials on the receiving spacecraft. It is shown that an uncertainty-based metric derived from the Extended Kalman Filter can be used to autonomously determine when the spacecraft should modify their pointing objectives to accommodate resource sharing. This uncertainty-based decision parameter enables the spacecraft to share information more efficiently than a fixed-measurement update schedule, by switching the tracking objective from a target mode to a sharing mode, only when needed. It is shown that a star tracker, or equivalent attitude determination system on the sharing spacecraft can accommodate the attitude measurement requirements of multiple spacecraft.
机译:本文调查了两个航天器之间的相对姿态共享的使用。首先,共享,航天器具有惯性姿态传感器。第二,接收,航天器缺乏态度传感器。共享航天器能够感测相对态度,从而能够确定接收航天器的惯性姿态与共享航天器的惯性姿态组成。假设仅在某些对准条件下可用的相对姿态与被动相对姿态传感器的适当取向一致,在接收航天器上的共享航天器和姿态基准上的被动相对姿态传感器。结果表明,从扩展卡尔曼滤波器导出的基于不确定性的度量可以用于自主地确定何时何时改变其指向目标以适应资源共享。基于不确定性的决策参数使得航天器能够通过将跟踪目标从目标模式切换到共享模式时更有效地共享信息,仅在需要时。结果表明,共用航天器上的星形跟踪器或同等姿态确定系统可以适应多个航天器的姿态测量要求。

著录项

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