首页> 外文会议>UKACC International Conference on Control >A survey of control strategies for spacecraft attitude and orientation
【24h】

A survey of control strategies for spacecraft attitude and orientation

机译:航天器态度与定位控制策略调查

获取原文

摘要

This paper presents a survey of different control methods deployed for spacecraft attitude control with a focus on strengths, weaknesses and opportunities for improvement. Common methods discussed include Sliding Mode Control (SMC), Unscented Kalman Filter (UKF) and Adaptive Control. Common challenges are the disturbances and uncertainties in space and produced by the spacecraft. This overview is used as a foundation for proposing useful research directions for developing improved control methods for the spacecraft attitude and orientation, with core requirements being low cost, robustness, precision, high efficiency and low computational load. The paper also summarises key actuation types used for satellite orientation, magnetics actuator and reaction wheels actuator, as the control strategy deployed, robustness and performance have strong links to the actuation.
机译:本文提出了对航天器态度控制部署的不同控制方法的调查,重点是优势,劣势和改进机会。讨论的常用方法包括滑模控制(SMC),Unscented Kalman滤波器(UKF)和自适应控制。共同挑战是太空中的紊乱和不确定性并由航天器生产。该概述被用作提出有用的研究方向,以提高用于开发改进的航天器姿态和方向的控制方法,具有核心需求,成本低,鲁棒性,精度,高效率和低计算负荷。本文还总结了用于卫星取向的关键致动类型,磁力执行器和反应轮执行器,因为部署的控制策略,鲁棒性和性能具有强烈的致动链接。

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