Three-axis stable electro-optical pod for unmanned aerial vehicle

A technology of three-axis stabilization and photoelectric pod, which is applied to aircraft parts, transportation and packaging, etc. It can solve the problems of increasing the difficulty of post-processing, affecting the shooting effect, blurring photos, etc., and achieves the effect of light weight, clear photos and small size

Active Publication Date: 2016-10-12
SHANGHAI AEROSPACE CONTROL TECH INST +1
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When using a high-resolution camera, due to factors such as vibration, yaw, pitch, and roll of the UAV platform during shooting, the photos taken will produce blur, distortion, and rotation, which will seriously affect the shooting effect and increase the post-production time. Difficulty of handling, how to overcome the above unfavorable factors has become a key technology that needs to be solved

Method used

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  • Three-axis stable electro-optical pod for unmanned aerial vehicle
  • Three-axis stable electro-optical pod for unmanned aerial vehicle
  • Three-axis stable electro-optical pod for unmanned aerial vehicle

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Embodiment Construction

[0027] Hereinafter, in conjunction with the accompanying drawings, a preferred embodiment is described in detail to further illustrate the present invention.

[0028] Such as figure 1 And combine Figure 2 ~ Figure 7 As shown, a three-axis stabilization photoelectric pod for unmanned aerial vehicles includes: a housing, and an azimuth axis assembly 100 arranged in the housing to provide an azimuth direction -180°~+180° rotation, and provide a pitch direction -180° A tilt axis assembly 200 that rotates by ~+180°, a roll axis assembly 300 that provides a rotation of -30°~+30° in a roll direction, and an image component 400 for taking photos; the azimuth axis assembly 100 is arranged in the housing In the upper space, the azimuth axis assembly 100 includes the azimuth axis bracket 104 and the azimuth axis drive motor 109, the azimuth axis transmission mechanism, the azimuth axis control board 103, and the azimuth axis system. The azimuth axis system includes The azimuth shaft beari...

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Abstract

The invention discloses a three-axis stable electro-optical pod for an unmanned aerial vehicle. The three-axis stable electro-optical pod comprises a shell, an azimuth axis assembly, a pitch axis assembly, a horizontal roller and an image assembly, wherein the azimuth axis assembly is arranged in the shell and provides rotation of -180 degrees to +180 degrees in the azimuth direction, the pitch axis assembly is arranged in the shell and provides rotation of -180 degrees to +180 degrees in the pitching direction, the horizontal roller provides rotation of -30 degrees to +30 degrees in the horizontal rolling direction, and the image assembly is used for shooting pictures. The three-axis stable electro-optical pod for the unmanned aerial vehicle is small in volume and light in weight and has a three-axis adjustment function, the pictures taken by the image assembly are clear and free of twist rotation.

Description

Technical field [0001] The invention relates to the field of optoelectronic technology, in particular to a three-axis stabilized optoelectronic pod for drones. Background technique [0002] With the wide application of UAVs in reconnaissance and surveillance, search and rescue, target positioning, identification and tracking, etc., the requirements for photoelectric pods are getting higher and higher. When using a high-resolution camera, due to the vibration, yaw, pitch and roll of the drone platform during shooting, the photos taken will be blurred, twisted, and rotated, which will seriously affect the shooting effect and increase the later stage. How to deal with the difficulty and how to overcome the above-mentioned disadvantages has become the key technology to be solved. Summary of the invention [0003] The purpose of the present invention is to provide a three-axis stabilized photoelectric pod for unmanned aerial vehicles, which is small in size, light in weight, has a thr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D47/08
CPCB64D47/08
Inventor 李洁冻贺亮曹涛黎枭金玲
Owner SHANGHAI AEROSPACE CONTROL TECH INST
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