• 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

固定翼自主飞行器机载传感器和相机的可定制随机高保真模型

Customizable Stochastic High-Fidelity Model of the Sensors and Camera Onboard a Fixed Wing Autonomous Aircraft.

作者信息

Gallo Eduardo, Barrientos Antonio

机构信息

Centro de Automática y Robótica, Universidad Politécnica de Madrid-Consejo Superior de Investigaciones, c/José Cutiérrez Abascal 2, 28006 Madrid, Spain.

出版信息

Sensors (Basel). 2022 Jul 24;22(15):5518. doi: 10.3390/s22155518.

DOI:10.3390/s22155518
PMID:35898024
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC9370995/
Abstract

The navigation systems of autonomous aircraft rely on the readings provided by a suite of onboard sensors to estimate the aircraft state. In the case of fixed wing vehicles, the sensor suite is usually composed by triads of accelerometers, gyroscopes, and magnetometers, a Global Navigation Satellite System (GNSS) receiver, and an air data system (Pitot tube, air vanes, thermometer, and barometer), and it is often complemented by one or more digital cameras. An accurate representation of the behavior and error sources of each of these sensors, together with the images generated by the cameras, is indispensable for the design, development, and testing of inertial, visual, or visual-inertial navigation algorithms. This article presents realistic and customizable models for each of these sensors; a ready-to-use C++ implementation is released as open-source code so non-experts in the field can easily generate realistic results. The pseudo-random models provide a time-stamped series of the errors generated by each sensor based on performance values and operating frequencies obtainable from the sensor's data sheets. If in addition, the simulated true pose (position plus attitude) of the aircraft is provided, the camera model generates realistic images of the Earth's surface that resemble those taken with a real camera from the same pose.

摘要

自主飞行器的导航系统依靠一套机载传感器提供的读数来估计飞行器状态。对于固定翼飞行器而言,传感器套件通常由加速度计、陀螺仪和磁力计三元组、全球导航卫星系统(GNSS)接收器以及一个大气数据系统(皮托管、风向标、温度计和气压计)组成,并且通常还会辅以一个或多个数码相机。准确描述这些传感器中每一个的行为和误差源,以及相机生成的图像,对于惯性、视觉或视觉惯性导航算法的设计、开发和测试而言是必不可少的。本文针对这些传感器中的每一个都给出了逼真且可定制的模型;一个即用型的C++实现版本作为开源代码发布,以便该领域的非专业人员能够轻松生成逼真的结果。伪随机模型基于可从传感器数据表中获取的性能值和工作频率,提供每个传感器产生的带有时间戳的误差序列。此外,如果提供了飞行器的模拟真实姿态(位置加姿态),相机模型会生成类似于从相同姿态用真实相机拍摄的地球表面的逼真图像。

相似文献

1
Customizable Stochastic High-Fidelity Model of the Sensors and Camera Onboard a Fixed Wing Autonomous Aircraft.固定翼自主飞行器机载传感器和相机的可定制随机高保真模型
Sensors (Basel). 2022 Jul 24;22(15):5518. doi: 10.3390/s22155518.
2
An innovative procedure for calibration of strapdown electro-optical sensors onboard unmanned air vehicles.一种创新的无人飞行器机载捷联式光电传感器校准方法。
Sensors (Basel). 2010;10(1):639-54. doi: 10.3390/s100100639. Epub 2010 Jan 18.
3
High Definition 3D Map Creation Using GNSS/IMU/LiDAR Sensor Integration to Support Autonomous Vehicle Navigation.利用全球导航卫星系统/惯性测量单元/激光雷达传感器集成创建高清3D地图以支持自动驾驶车辆导航。
Sensors (Basel). 2020 Feb 7;20(3):899. doi: 10.3390/s20030899.
4
Magnetometer-augmented IMU simulator: in-depth elaboration.磁力计增强型惯性测量单元模拟器:深入阐述。
Sensors (Basel). 2015 Mar 4;15(3):5293-310. doi: 10.3390/s150305293.
5
An Algorithm for Online Stochastic Error Modeling of Inertial Sensors in Urban Cities.城市环境中惯性传感器在线随机误差建模算法。
Sensors (Basel). 2023 Jan 21;23(3):1257. doi: 10.3390/s23031257.
6
Real-Time Onboard 3D State Estimation of an Unmanned Aerial Vehicle in Multi-Environments Using Multi-Sensor Data Fusion.基于多传感器数据融合的无人机在多环境中的实时机载三维状态估计
Sensors (Basel). 2020 Feb 9;20(3):919. doi: 10.3390/s20030919.
7
Performance Enhancement of Consumer-Grade MEMS Sensors through Geometrical Redundancy.通过几何冗余提高消费级 MEMS 传感器的性能。
Sensors (Basel). 2021 Jul 16;21(14):4851. doi: 10.3390/s21144851.
8
Benefits of Multi-Constellation/Multi-Frequency GNSS in a Tightly Coupled GNSS/IMU/Odometry Integration Algorithm.多星座/多频率 GNSS 在紧耦合 GNSS/IMU/里程计组合算法中的优势。
Sensors (Basel). 2018 Sep 12;18(9):3052. doi: 10.3390/s18093052.
9
Performance Characterization of GNSS/IMU/DVL Integration under Real Maritime Jamming Conditions.GNSS/IMU/DVL 集成在真实海况干扰下的性能特征分析。
Sensors (Basel). 2018 Sep 5;18(9):2954. doi: 10.3390/s18092954.
10
Monocular camera/IMU/GNSS integration for ground vehicle navigation in challenging GNSS environments.单目相机/惯性测量单元/全球导航卫星系统集成在挑战性的全球导航卫星系统环境中用于地面车辆导航。
Sensors (Basel). 2012;12(3):3162-85. doi: 10.3390/s120303162. Epub 2012 Mar 7.

本文引用的文献

1
Strapdown Inertial Navigation Systems for Positioning Mobile Robots-MEMS Gyroscopes Random Errors Analysis Using Allan Variance Method.用于移动机器人定位的捷联惯性导航系统——基于阿伦方差法的MEMS陀螺仪随机误差分析
Sensors (Basel). 2020 Aug 27;20(17):4841. doi: 10.3390/s20174841.
2
On the Error State Selection for Stationary SINS Alignment and Calibration Kalman Filters-Part II: Observability/Estimability Analysis.关于静态捷联惯性导航系统对准与校准卡尔曼滤波器的误差状态选择 - 第二部分:可观测性/可估计性分析
Sensors (Basel). 2017 Feb 23;17(3):439. doi: 10.3390/s17030439.
3
On the Design of Attitude-Heading Reference Systems Using the Allan Variance.
基于阿伦方差的姿态航向参考系统设计
IEEE Trans Ultrason Ferroelectr Freq Control. 2016 Apr;63(4):656-65. doi: 10.1109/TUFFC.2016.2519268. Epub 2016 Jan 19.
4
Online estimation of Allan variance coefficients based on a neural-extended Kalman filter.基于神经扩展卡尔曼滤波器的阿伦方差系数在线估计
Sensors (Basel). 2015 Jan 23;15(2):2496-524. doi: 10.3390/s150202496.
5
A comparison between different error modeling of MEMS applied to GPS/INS integrated systems.不同误差建模方法在 GPS/INS 组合系统中应用的比较。
Sensors (Basel). 2013 Jul 24;13(8):9549-88. doi: 10.3390/s130809549.