基于不确定性深度学习的轴对称物体六自由度姿态估计

Shintaro Hashimoto, Daichi Hirano, N. Ishihama
{"title":"基于不确定性深度学习的轴对称物体六自由度姿态估计","authors":"Shintaro Hashimoto, Daichi Hirano, N. Ishihama","doi":"10.1109/AERO47225.2020.9172298","DOIUrl":null,"url":null,"abstract":"Before space debris can be removed efficiently, its 6-DoF poses (positions and attitudes) need to be estimated accurately from observed images with high resolution. Further, if the debris is axisymmetric, such as the remains of a multistage rocket, or if part of the debris cannot be seen due to optical conditions, it is considerably more difficult to estimate its parameters. If some parameters cannot be estimated for some reason, all parameters may be affected because each parameter in Euler angle and quaternion has an interdependency and the solution will not be determined uniquely. This research proposes methods that obtain the solution by decomposing the quaternion into the direction and rotation based on the forward direction so that direction and rotation parameters can be estimated independently. Moreover, this research was able to adaptively improve accuracy based on a threshold of uncertainty by adding an uncertainty value to each parameter. When the estimated parameters likely having error values that exceed 2% based on uncertainty value are deleted, estimated error of parameter $x, y, z$ (position), $n_{x}, n_{y},n_{z}$ and $\\theta_{z}$ (attitude) were 1.25%, 1.35%, 3.76%, 2.27%, 2.64%, 3.06%, and 18.32% respectively.","PeriodicalId":114560,"journal":{"name":"2020 IEEE Aerospace Conference","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"6-DoF Pose Estimation for Axisymmetric Objects Using Deep Learning with Uncertainty\",\"authors\":\"Shintaro Hashimoto, Daichi Hirano, N. Ishihama\",\"doi\":\"10.1109/AERO47225.2020.9172298\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Before space debris can be removed efficiently, its 6-DoF poses (positions and attitudes) need to be estimated accurately from observed images with high resolution. Further, if the debris is axisymmetric, such as the remains of a multistage rocket, or if part of the debris cannot be seen due to optical conditions, it is considerably more difficult to estimate its parameters. If some parameters cannot be estimated for some reason, all parameters may be affected because each parameter in Euler angle and quaternion has an interdependency and the solution will not be determined uniquely. This research proposes methods that obtain the solution by decomposing the quaternion into the direction and rotation based on the forward direction so that direction and rotation parameters can be estimated independently. Moreover, this research was able to adaptively improve accuracy based on a threshold of uncertainty by adding an uncertainty value to each parameter. When the estimated parameters likely having error values that exceed 2% based on uncertainty value are deleted, estimated error of parameter $x, y, z$ (position), $n_{x}, n_{y},n_{z}$ and $\\\\theta_{z}$ (attitude) were 1.25%, 1.35%, 3.76%, 2.27%, 2.64%, 3.06%, and 18.32% respectively.\",\"PeriodicalId\":114560,\"journal\":{\"name\":\"2020 IEEE Aerospace Conference\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-03-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 IEEE Aerospace Conference\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/AERO47225.2020.9172298\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 IEEE Aerospace Conference","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/AERO47225.2020.9172298","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1

摘要

在有效清除空间碎片之前,需要从高分辨率的观测图像中准确估计其六自由度姿态(位置和姿态)。此外,如果碎片是轴对称的,例如多级火箭的残骸,或者由于光学条件无法看到部分碎片,则估计其参数要困难得多。如果某些参数由于某种原因无法估计,那么由于欧拉角和四元数中的每个参数都具有相互依赖性,不能唯一确定解,可能会影响所有参数。本研究提出了基于正向将四元数分解为方向和旋转的求解方法,从而可以独立估计方向和旋转参数。此外,本研究能够通过在每个参数中添加不确定值,自适应地提高基于不确定阈值的精度。剔除不确定度估计误差值可能超过2%的参数后,参数$x、y、z$(位置)、$n_{x}、n_{y}、n_{z}$和$\theta_{z}$(姿态)的估计误差分别为1.25%、1.35%、3.76%、2.27%、2.64%、3.06%和18.32%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
6-DoF Pose Estimation for Axisymmetric Objects Using Deep Learning with Uncertainty
Before space debris can be removed efficiently, its 6-DoF poses (positions and attitudes) need to be estimated accurately from observed images with high resolution. Further, if the debris is axisymmetric, such as the remains of a multistage rocket, or if part of the debris cannot be seen due to optical conditions, it is considerably more difficult to estimate its parameters. If some parameters cannot be estimated for some reason, all parameters may be affected because each parameter in Euler angle and quaternion has an interdependency and the solution will not be determined uniquely. This research proposes methods that obtain the solution by decomposing the quaternion into the direction and rotation based on the forward direction so that direction and rotation parameters can be estimated independently. Moreover, this research was able to adaptively improve accuracy based on a threshold of uncertainty by adding an uncertainty value to each parameter. When the estimated parameters likely having error values that exceed 2% based on uncertainty value are deleted, estimated error of parameter $x, y, z$ (position), $n_{x}, n_{y},n_{z}$ and $\theta_{z}$ (attitude) were 1.25%, 1.35%, 3.76%, 2.27%, 2.64%, 3.06%, and 18.32% respectively.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
An Integrated Innovative 3D Radiation Protection Fabric for Advanced Spacesuits and Systems Model-based Tools designed for the FACE™ Technical Standard, Editions 3.0 & 2.1 Can Adaptive Response and Evolution Make Survival of Extremophile Bacteria Possible on Mars? Initial Orbit Determination Using Simplex Fusion Headline-based visualization to prioritize events
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1