吉林大学学报(工学版)2024,Vol.54Issue(8) :2130-2140.DOI:10.13229/j.cnki.jdxbgxb.20230894

面向分体式飞行汽车对接锁定的机电系统设计与验证

Design and verification of electromechanical system for docking and locking of modular flying vehicle

王琛 雒特 惠倩倩 王忠昊 王方方
吉林大学学报(工学版)2024,Vol.54Issue(8) :2130-2140.DOI:10.13229/j.cnki.jdxbgxb.20230894

面向分体式飞行汽车对接锁定的机电系统设计与验证

Design and verification of electromechanical system for docking and locking of modular flying vehicle

王琛 1雒特 1惠倩倩 1王忠昊 1王方方1
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作者信息

  • 1. 长安大学工程机械学院,西安 710064
  • 折叠

摘要

采用"型面滑动导引+多点锁定"的思想设计对接机构的方案,依据捕获域理论和动力学仿真进行对接过程的静态/动态分析,建立缩比试验平台并进行多科目的对接锁定试验,验证了分体式飞行汽车对接的可靠性、稳定性和快速性.通过控制通信系统与机械导引,分体式飞行汽车能够完成水平偏差±100 mm、航向偏差±5°条件下的位姿校正并实现可靠的多点对接锁紧,试验结果表明:该对接系统能够准确、稳定和快速地进行模态切换.

Abstract

The design of the docking and locking system scheme adopted the concept of"profile sliding guidance+multi-point locking".Static and dynamic analyses of the docking process were conducted using the capture domain theory and dynamic simulations.A scaled-down experimental platform was established for multi-objective docking and locking tests,thus confirming the reliability,stability,and speed of the modular flying vehicle.By controlling the communication system and mechanical guidance,the modular flying vehicle can achieve pose correction under conditions of horizontal deviation within a range of±10 mm and heading deviation within a range of±5 degrees.Experimental results indicate that this docking system ensures the accuracy,stability,and swiftness of module transitions during modal switching.

关键词

机械设计及理论/分体式飞行汽车/机电系统/模块化设计/捕获域

Key words

mechanical design and theory/modular flying vehicle/electromechanical system/modular design/capture domain

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出版年

2024
吉林大学学报(工学版)
吉林大学

吉林大学学报(工学版)

CSTPCD北大核心
影响因子:0.792
ISSN:1671-5497
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