多旋翼飞行器编队运输悬挂物的建模、仿真与控制

Elia Costantini
{"title":"多旋翼飞行器编队运输悬挂物的建模、仿真与控制","authors":"Elia Costantini","doi":"10.1007/s42496-023-00192-3","DOIUrl":null,"url":null,"abstract":"<div><p>This work aims to contribute to the innovation in the urban air mobility and delivery sector and represents a starting point for air logistics and its future scenarios. The dissertation focuses on modeling, simulation, and control of a formation of multirotor aircraft for cooperative load transportation, with particular attention to the stabilization of payload swing motion. Starting from the mathematical model of two identical multirotors, formation-flight-keeping and collision-avoidance algorithms are implemented to ensure the safety of the vehicles within the formation and that of the payload. Then, a mathematical model for the suspended load is implemented, as well as an active controller for its stabilization. The focus of this section is thus represented by the analysis of payload oscillatory motion, whose kinetic energy decay is investigated. Several test cases are presented to establish the most effective and safe strategy in light of future aerospace applications.</p></div>","PeriodicalId":100054,"journal":{"name":"Aerotecnica Missili & Spazio","volume":"103 3","pages":"233 - 244"},"PeriodicalIF":0.0000,"publicationDate":"2023-12-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Modeling, Simulation, and Control of a Formation of Multirotor Aircraft for Transportation of Suspended Loads\",\"authors\":\"Elia Costantini\",\"doi\":\"10.1007/s42496-023-00192-3\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>This work aims to contribute to the innovation in the urban air mobility and delivery sector and represents a starting point for air logistics and its future scenarios. The dissertation focuses on modeling, simulation, and control of a formation of multirotor aircraft for cooperative load transportation, with particular attention to the stabilization of payload swing motion. Starting from the mathematical model of two identical multirotors, formation-flight-keeping and collision-avoidance algorithms are implemented to ensure the safety of the vehicles within the formation and that of the payload. Then, a mathematical model for the suspended load is implemented, as well as an active controller for its stabilization. The focus of this section is thus represented by the analysis of payload oscillatory motion, whose kinetic energy decay is investigated. Several test cases are presented to establish the most effective and safe strategy in light of future aerospace applications.</p></div>\",\"PeriodicalId\":100054,\"journal\":{\"name\":\"Aerotecnica Missili & Spazio\",\"volume\":\"103 3\",\"pages\":\"233 - 244\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2023-12-15\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerotecnica Missili & Spazio\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s42496-023-00192-3\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerotecnica Missili & Spazio","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.1007/s42496-023-00192-3","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

摘要

这项工作旨在为城市空中交通和运输领域的创新做出贡献,是空中物流及其未来方案的起点。论文的重点是多旋翼飞行器编队的建模、仿真和控制,以实现合作载荷运输,尤其关注有效载荷摆动运动的稳定性。从两个相同多旋翼飞行器的数学模型开始,实施编队飞行保持和避免碰撞算法,以确保编队内飞行器和有效载荷的安全。然后,实施悬挂载荷的数学模型以及用于稳定载荷的主动控制器。因此,本节的重点是分析有效载荷的摆动运动,研究其动能衰减。本节介绍了几个测试案例,以便根据未来的航空航天应用确定最有效、最安全的策略。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Modeling, Simulation, and Control of a Formation of Multirotor Aircraft for Transportation of Suspended Loads

Modeling, Simulation, and Control of a Formation of Multirotor Aircraft for Transportation of Suspended Loads

This work aims to contribute to the innovation in the urban air mobility and delivery sector and represents a starting point for air logistics and its future scenarios. The dissertation focuses on modeling, simulation, and control of a formation of multirotor aircraft for cooperative load transportation, with particular attention to the stabilization of payload swing motion. Starting from the mathematical model of two identical multirotors, formation-flight-keeping and collision-avoidance algorithms are implemented to ensure the safety of the vehicles within the formation and that of the payload. Then, a mathematical model for the suspended load is implemented, as well as an active controller for its stabilization. The focus of this section is thus represented by the analysis of payload oscillatory motion, whose kinetic energy decay is investigated. Several test cases are presented to establish the most effective and safe strategy in light of future aerospace applications.

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
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信