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预置式筒射四旋翼无人机设计及发射控制技术

张浩哲 袁祖江 刘璐 孔帅帅 王琦 温竞龙 齐向东 刘丹

测试技术学报2026,Vol.40Issue(2):193-204,12.
测试技术学报2026,Vol.40Issue(2):193-204,12.DOI:10.62756/csjs.1671-7449.2026040

预置式筒射四旋翼无人机设计及发射控制技术

Design of Pre-Embedded Tube-Launched Multi-Rotor UAV and Launch Control Technology

张浩哲 1袁祖江 1刘璐 1孔帅帅 1王琦 1温竞龙 1齐向东 1刘丹1

作者信息

  • 1. 中北大学 极限环境光电动态测试技术与仪器全国重点实验室,山西 太原 030051
  • 折叠

摘要

Abstract

To address the technological gap in the full-process autonomous operation of"pre-deployment-activation-flight"for traditional tube-launched multirotor UAVs in complex water-air cross-media envi-ronments,a pre-deployed tube-launched quadrotor aircraft named Feiying is proposed,aiming to overcome the limitations of traditional systems in response latency and single-stage control and to meet the demands for long-duration pre-deployment,rapid activation,and fast response in complex environments.In this scheme,an innovative carbon-fiber/aluminum-alloy composite load-bearing structure and a torsion-spring-driven folding-wing mechanism are employed,and a hierarchical power-supply system is integrated with a state-machine-based full-process control model.Validation results indicate that Feiying can maintain low-power standby while being rapidly activated into its mission state and can quickly transition to autonomous flight mode during launch,demonstrating a reliable 30 d pre-deployment capability and a rapid response time of 0.1 s.This design achieves highly reliable deployment and high-speed responsiveness for pre-deployed tube-launched quadrotor UAVs and provides a technical foundation and verification support for subsequent engineering applications.

关键词

四旋翼无人机/预置式发射/复合结构/折叠机构/分级供能

Key words

quadcopter/pre-deployment launch/composite structure/folding mechanism/hierarchical power supply

分类

航空航天

引用本文复制引用

张浩哲,袁祖江,刘璐,孔帅帅,王琦,温竞龙,齐向东,刘丹..预置式筒射四旋翼无人机设计及发射控制技术[J].测试技术学报,2026,40(2):193-204,12.

基金项目

中央引导地方科技发展基金资助项目(2025090) (2025090)

山西省科技创新团队专项资金资助项目(202304051001030) (202304051001030)

山西省回国留学人员科研资助项目(2022-144) (2022-144)

山西省基础研究计划资助项目(202303021222119) (202303021222119)

测试技术学报

1671-7449

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