固定翼无人机发射架及发射方法
By combining angle and pitch adjustment mechanisms with friction wheel launch, the launch direction and speed of the UAV can be adjusted in real time, solving the problem of high difficulty in UAV formation in existing technologies and realizing rapid and accurate launch of UAV formations.
CN118182912BActive Publication Date: 2026-07-17CIVIL AVIATION UNIV OF CHINA
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- CIVIL AVIATION UNIV OF CHINA
- Filing Date
- 2024-04-22
- Publication Date
- 2026-07-17
AI Technical Summary
Technical Problem
Existing fixed-wing UAV launchers cannot adjust the launch direction, launch angle, and speed in real time, making UAV formation difficult and incompatible with different UAV models.
Method used
By employing an angle adjustment mechanism and a pitch adjustment mechanism, combined with a friction wheel launch mechanism, and using an industrial camera to capture the trajectory of aerial objects in real time, the launch direction, pitch angle, and speed can be flexibly adjusted to achieve precise formation of UAVs.
Benefits of technology
It reduces the difficulty of drone aerial formation, improves the compatibility and adaptability of the launcher, and enables the rapid completion of drone formation.
✦ Generated by Eureka AI based on patent content.
Smart Images
Figure CN118182912B_ABST
Abstract
本发明涉及无人机发射技术领域，具体涉及一种固定翼无人机发射架及发射方法，包括：无人机托板、摩擦轮发射机构、底盘、角度调节机构、俯仰调节机构、工业摄像机和控制器，其中，所述摩擦轮发射机构包括两组摩擦轮，使得两组所述摩擦轮之间形成发射通道，所述摩擦轮设置为转速可调；利用工业摄像机实时捕捉空中飞行物，结合算法计算出角度调节机构、俯仰调节机构所需要调整的角度，以及摩擦轮发射机构的发射速度，并实时调整发射方向、发射俯仰角和发射速度，通过多组摩擦轮将无人机以设定发射方向、发射俯仰角以及速度发射至空中的预定位置，快速完成无人机编队，降低无人机空中编队的难度。
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