• 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

基于斐波那契搜索算法的无人机控制器无模型实时最小寻优自整定方法。

Real-Time Model-Free Minimum-Seeking Autotuning Method for Unmanned Aerial Vehicle Controllers Based on Fibonacci-Search Algorithm.

机构信息

Institute of Control, Robotics and Information Engineering, Poznan University of Technology, Piotrowo 3a, 60-965 Poznan, Poland.

Department of Cybernetics, Faculty of Electrical Engineering, Czech Technical University in Prague, Technicka 2, 166 27 Prague 6, Czech Republic.

出版信息

Sensors (Basel). 2019 Jan 14;19(2):312. doi: 10.3390/s19020312.

DOI:10.3390/s19020312
PMID:30646579
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC6359052/
Abstract

The paper presents a novel autotuning approach for finding locally-best parameters of controllers on board of unmanned aerial vehicles (UAVs). The controller tuning is performed fully autonomously during flight on the basis of predefined ranges of controller parameters. Required controller properties may be simply interpreted by a cost function, which is involved in the optimization process. For example, the sum of absolute values of the tracking error samples or performance indices, including weighed functions of control signal samples, can be penalized to achieve very precise position control, if required. The proposed method relies on an optimization procedure using Fibonacci-search technique fitted into bootstrap sequences, enabling one to obtain a global minimizer for a unimodal cost function. The approach is characterized by low computational complexity and does not require any UAV dynamics model (just periodical measurements from basic onboard sensors) to obtain proper tuning of a controller. In addition to the theoretical background of the method, an experimental verification in real-world outdoor conditions is provided. The experiments have demonstrated a high robustness of the method to in-environment disturbances, such as wind, and its easy deployability.

摘要

本文提出了一种新颖的自动调谐方法,用于在无人机(UAV)上找到控制器的局部最佳参数。控制器调谐在飞行过程中完全自主进行,基于控制器参数的预定义范围。所需的控制器属性可以通过成本函数简单解释,该函数参与优化过程。例如,如果需要,可以对跟踪误差样本或性能指标的绝对值(包括控制信号样本的加权函数)进行惩罚,以实现非常精确的位置控制。所提出的方法依赖于使用 Fibonacci 搜索技术拟合到自举序列中的优化过程,从而能够获得单峰成本函数的全局最小值。该方法的特点是计算复杂度低,并且不需要任何无人机动力学模型(只需从基本的机载传感器进行周期性测量)即可实现控制器的适当调谐。除了该方法的理论背景外,还提供了在真实户外条件下的实验验证。实验表明,该方法对环境干扰(如风)具有很高的鲁棒性,并且易于部署。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/5b0c371affc8/sensors-19-00312-g019.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d8328035dd43/sensors-19-00312-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/1ed8de4e1280/sensors-19-00312-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/200e387fa8d6/sensors-19-00312-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d26dbb2e19f2/sensors-19-00312-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/4b712cbb8540/sensors-19-00312-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/bab797f2c567/sensors-19-00312-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/38dcbf69aec8/sensors-19-00312-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/9c897b2548c3/sensors-19-00312-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d30ebd00027d/sensors-19-00312-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/85c0c113d600/sensors-19-00312-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/10834fbfa99e/sensors-19-00312-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/b3ce534a7124/sensors-19-00312-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/672db35ae7fa/sensors-19-00312-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d7b44db99409/sensors-19-00312-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/fab5b99e4312/sensors-19-00312-g015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d2daccf82938/sensors-19-00312-g016.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/1bd47648ab66/sensors-19-00312-g017.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/ed1e06d0e815/sensors-19-00312-g018.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/5b0c371affc8/sensors-19-00312-g019.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d8328035dd43/sensors-19-00312-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/1ed8de4e1280/sensors-19-00312-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/200e387fa8d6/sensors-19-00312-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d26dbb2e19f2/sensors-19-00312-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/4b712cbb8540/sensors-19-00312-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/bab797f2c567/sensors-19-00312-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/38dcbf69aec8/sensors-19-00312-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/9c897b2548c3/sensors-19-00312-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d30ebd00027d/sensors-19-00312-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/85c0c113d600/sensors-19-00312-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/10834fbfa99e/sensors-19-00312-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/b3ce534a7124/sensors-19-00312-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/672db35ae7fa/sensors-19-00312-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d7b44db99409/sensors-19-00312-g014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/fab5b99e4312/sensors-19-00312-g015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/d2daccf82938/sensors-19-00312-g016.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/1bd47648ab66/sensors-19-00312-g017.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/ed1e06d0e815/sensors-19-00312-g018.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1fa2/6359052/5b0c371affc8/sensors-19-00312-g019.jpg

相似文献

1
Real-Time Model-Free Minimum-Seeking Autotuning Method for Unmanned Aerial Vehicle Controllers Based on Fibonacci-Search Algorithm.基于斐波那契搜索算法的无人机控制器无模型实时最小寻优自整定方法。
Sensors (Basel). 2019 Jan 14;19(2):312. doi: 10.3390/s19020312.
2
Development of Model Predictive Controller for a Tail-Sitter VTOL UAV in Hover Flight.尾座式垂直起降无人机悬停飞行的模型预测控制器的开发。
Sensors (Basel). 2018 Aug 30;18(9):2859. doi: 10.3390/s18092859.
3
Optimal tuning of fractional-order controllers based on Fibonacci-search method.基于斐波那契搜索法的分数阶控制器的最优整定
ISA Trans. 2020 Sep;104:287-298. doi: 10.1016/j.isatra.2020.05.022. Epub 2020 May 18.
4
Auto-landing of fixed wing unmanned aerial vehicles using the backstepping control.固定翼无人机的自动着陆采用反推控制。
ISA Trans. 2019 Dec;95:194-210. doi: 10.1016/j.isatra.2019.05.019. Epub 2019 May 29.
5
Autonomous Unmanned Aerial Vehicles in Search and Rescue Missions Using Real-Time Cooperative Model Predictive Control.自主式无人机在搜救任务中的应用——基于实时协同模型预测控制
Sensors (Basel). 2019 Sep 20;19(19):4067. doi: 10.3390/s19194067.
6
Differential-Evolution Control Parameter Optimization for Unmanned Aerial Vehicle Path Planning.用于无人机路径规划的差分进化控制参数优化
PLoS One. 2016 Mar 4;11(3):e0150558. doi: 10.1371/journal.pone.0150558. eCollection 2016.
7
Integrated optimization of unmanned aerial vehicle task allocation and path planning under steady wind.稳态风下无人机任务分配与路径规划的综合优化。
PLoS One. 2018 Mar 21;13(3):e0194690. doi: 10.1371/journal.pone.0194690. eCollection 2018.
8
Autonomous Vision-Based Aerial Grasping for Rotorcraft Unmanned Aerial Vehicles.基于视觉的旋翼机无人机自主空中抓取
Sensors (Basel). 2019 Aug 3;19(15):3410. doi: 10.3390/s19153410.
9
A Decentralized Low-Chattering Sliding Mode Formation Flight Controller for a Swarm of UAVs.一种用于无人机群的分布式低抖振滑模编队飞行控制器。
Sensors (Basel). 2020 May 30;20(11):3094. doi: 10.3390/s20113094.
10
System Identification and Nonlinear Model Predictive Control with Collision Avoidance Applied in Hexacopters UAVs.应用于六旋翼无人机的系统辨识与带避碰功能的非线性模型预测控制
Sensors (Basel). 2022 Jun 22;22(13):4712. doi: 10.3390/s22134712.

引用本文的文献

1
Altitude Measurement-Based Optimization of the Landing Process of UAVs.基于海拔测量的无人机着陆过程优化。
Sensors (Basel). 2021 Feb 6;21(4):1151. doi: 10.3390/s21041151.