• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

基于指数坐标的一组刚体姿态同步

Attitude Synchronization of a Group of Rigid Bodies Using Exponential Coordinates.

作者信息

Sidón-Ayala Miguel, Pliego-Jiménez Javier, Cruz-Hernandez César

机构信息

Departamento de Electrónica y Telecomunicaciones, División de Física Aplicada, Centro de Investigación Científica y de Educación Superior de Ensenada, Carretera Ensenada-Tijuana 3918, Ensenada 22860, Mexico.

Programa Investigadores por México, Consejo Nacional de Humanidades Ciencias y Tecnologías, Av. Insurgentes Sur 1582, Mexico City 03940, Mexico.

出版信息

Entropy (Basel). 2023 May 23;25(6):832. doi: 10.3390/e25060832.

DOI:10.3390/e25060832
PMID:37372176
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC10296865/
Abstract

Currently, managing a group of satellites or robot manipulators requires coordinating their motion and work in a cooperative way to complete complex tasks. The attitude motion coordination and synchronization problems are challenging since attitude motion evolves in non-Euclidean spaces. Moreover, the equation of motions of the rigid body are highly nonlinear. This paper studies the attitude synchronization problem of a group of fully actuated rigid bodies over a directed communication topology. To design the synchronization control law, we exploit the cascade structure of the rigid body's kinematic and dynamic models. First, we propose a kinematic control law that induces attitude synchronization. As a second step, an angular velocity-tracking control law is designed for the dynamic subsystem. We use the exponential coordinates of rotation to describe the body's attitude. Such coordinates are a natural and minimal parametrization of rotation matrices which almost describe every rotation on the Special Orthogonal group SO(3). We provide simulation results to show the performance of the proposed synchronization controller.

摘要

目前,管理一组卫星或机器人操纵器需要以协作的方式协调它们的运动和工作,以完成复杂任务。姿态运动协调和同步问题具有挑战性,因为姿态运动在非欧几里得空间中演化。此外,刚体的运动方程是高度非线性的。本文研究了在有向通信拓扑结构下一组全驱动刚体的姿态同步问题。为了设计同步控制律,我们利用了刚体运动学和动力学模型的级联结构。首先,我们提出了一种诱导姿态同步的运动学控制律。第二步,为动态子系统设计了角速度跟踪控制律。我们使用旋转的指数坐标来描述物体的姿态。这样的坐标是旋转矩阵的一种自然且最小的参数化,它几乎描述了特殊正交群SO(3)上的每一种旋转。我们提供了仿真结果来展示所提出的同步控制器的性能。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/68f1c198d8a2/entropy-25-00832-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/9f0291523938/entropy-25-00832-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/a42404504dbd/entropy-25-00832-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/14eac80b676c/entropy-25-00832-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/906791dc2b06/entropy-25-00832-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/e8bef71e165d/entropy-25-00832-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/be31a5ed15ce/entropy-25-00832-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/65de413b7eb1/entropy-25-00832-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/68f1c198d8a2/entropy-25-00832-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/9f0291523938/entropy-25-00832-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/a42404504dbd/entropy-25-00832-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/14eac80b676c/entropy-25-00832-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/906791dc2b06/entropy-25-00832-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/e8bef71e165d/entropy-25-00832-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/be31a5ed15ce/entropy-25-00832-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/65de413b7eb1/entropy-25-00832-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a9c6/10296865/68f1c198d8a2/entropy-25-00832-g008.jpg

相似文献

1
Attitude Synchronization of a Group of Rigid Bodies Using Exponential Coordinates.基于指数坐标的一组刚体姿态同步
Entropy (Basel). 2023 May 23;25(6):832. doi: 10.3390/e25060832.
2
Synchronization of multiple rigid body systems: A survey.多刚体系统的同步:综述
Chaos. 2023 Sep 1;33(9). doi: 10.1063/5.0156301.
3
Hybrid triggering design for global attitude synchronization of networked rigid bodies.用于网络化刚体全局姿态同步的混合触发设计
ISA Trans. 2023 Nov;142:188-197. doi: 10.1016/j.isatra.2023.07.016. Epub 2023 Jul 18.
4
Attitude output feedback control for rigid spacecraft with finite-time convergence.具有有限时间收敛性的刚体航天器姿态输出反馈控制
ISA Trans. 2017 Sep;70:173-186. doi: 10.1016/j.isatra.2017.07.023. Epub 2017 Aug 5.
5
Attitude-Orbit Coupled Control of Gravitational Wave Detection Spacecraft with Communication Delays.带有通信时滞的引力波探测航天器的姿态-轨道耦合控制。
Sensors (Basel). 2023 Mar 17;23(6):3233. doi: 10.3390/s23063233.
6
Velocity-Free Leader-Follower Cooperative Attitude Tracking of Multiple Rigid Bodies on SO(3).基于 SO(3)的多刚体速度自由领导者-跟随者协同姿态跟踪。
IEEE Trans Cybern. 2019 Dec;49(12):4078-4089. doi: 10.1109/TCYB.2018.2857008. Epub 2018 Dec 20.
7
Decentralized finite-time attitude synchronization for multiple rigid spacecraft via a novel disturbance observer.基于新型干扰观测器的多刚体航天器分布式有限时间姿态同步
ISA Trans. 2016 Nov;65:150-163. doi: 10.1016/j.isatra.2016.08.009. Epub 2016 Sep 13.
8
Fixed-time attitude coordination control for spacecraft with external disturbance.具有外部干扰的航天器固定时间姿态协调控制
ISA Trans. 2021 Aug;114:150-170. doi: 10.1016/j.isatra.2020.12.048. Epub 2020 Dec 28.
9
Robust tracking and distributed synchronization control of a multi-motor servomechanism with H-infinity performance.多电机伺服机构的鲁棒跟踪与分布式同步 H-infinity 性能控制
ISA Trans. 2018 Jan;72:147-160. doi: 10.1016/j.isatra.2017.09.018. Epub 2017 Oct 21.
10
Rotation matrix based finite-time attitude synchronization control for spacecraft with external disturbances.基于旋转矩阵的具有外部干扰的航天器有限时间姿态同步控制。
ISA Trans. 2019 Feb;85:141-150. doi: 10.1016/j.isatra.2018.10.027. Epub 2018 Oct 27.