预置式筒射四旋翼无人机设计及发射控制技术OA
Design of Pre-Embedded Tube-Launched Multi-Rotor UAV and Launch Control Technology
针对在水空跨介质的复杂环境下,传统筒射多旋翼无人机在"预置-激活-飞行"全流程自主运行方面的技术空白,提出一种预置式筒射四旋翼飞行器"飞影",旨在突破传统系统响应延迟与单一阶段控制的局限,满足复杂环境中长时间预置、快速激活及响应的需求.该方案创新采用碳纤维-铝合金复合承力结构与扭簧驱动折叠机翼机制,融合分级供能系统与基于状态机的全流程控制模型.验证结果表明,"飞影"在实现低功耗待机的同时可快速激活进入任务状态,发射时能快速切换至自主飞行状态,具备30 d可靠预置能力与0.1 s快速响应能力.该设计方案实现了预置发射四旋翼无人机的高可靠部署与高速响应能力,为后续工程应用提供技术基础与验证支撑.
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.
张浩哲;袁祖江;刘璐;孔帅帅;王琦;温竞龙;齐向东;刘丹
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
航空航天
四旋翼无人机预置式发射复合结构折叠机构分级供能
quadcopterpre-deployment launchcomposite structurefolding mechanismhierarchical power supply
《测试技术学报》 2026 (2)
193-204,12
中央引导地方科技发展基金资助项目(2025090)山西省科技创新团队专项资金资助项目(202304051001030)山西省回国留学人员科研资助项目(2022-144)山西省基础研究计划资助项目(202303021222119)
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