Three-axis aerial measurement tripod head special for steering engine drive catapult take-off unmanned aerial vehicle

A servo-driven, unmanned aerial vehicle technology, applied in the field of gimbals, can solve the problems of not working normally, and the camera can not always be aimed at the shooting object, etc.

Inactive Publication Date: 2016-12-07
南昌白龙马航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the camera is fixed, when the aircraft produces a pitch angle, yaw angle or r

Method used

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  • Three-axis aerial measurement tripod head special for steering engine drive catapult take-off unmanned aerial vehicle
  • Three-axis aerial measurement tripod head special for steering engine drive catapult take-off unmanned aerial vehicle

Examples

Experimental program
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Example Embodiment

[0015] Example one

[0016] As attached figure 1 , 2 As shown, a steering gear-driven three-axis aerial survey platform for catapult take-off drones includes a base 1, a lower bracket 2 is fixed on the base 1, and the lower bracket 2 is hinged with a pitch correction bracket through a pitch correction rotation axis 3 4. The pitch correction bracket 4 is hinged to the camera fixing bracket 6 through the roll correction rotation axis 5, the camera fixing bracket 6 is fixed with a SLR camera 7, and the lens of the SLR camera 7 is provided with a yaw correction Rotating mechanism 8, the pitch correction rotating shaft 3 is provided with a pitch correction steering gear mechanism, the roll correction rotating shaft 5 is provided with a roll correction steering gear mechanism, and the yaw correction rotating mechanism 8 is linked The yaw correction rotary steering gear 14 is arranged on the top of the camera fixing bracket 6.

[0017] The pitch correction steering gear mechanism of this...

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PUM

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Abstract

The invention relates to a tripod head, in particular to a three-axis aerial measurement tripod head special for a steering engine drive catapult take-off unmanned aerial vehicle. The structure of the tripod head comprises a base. A lower bracket is fixed to the upper portion of the base. A pitching correction bracket is hinged to the lower bracket through a pitching correction rotating shaft. A camera fixing bracket is hinged to the pitching correction bracket through a rolling correction rotating shaft. A single lens reflex camera is fixed to the camera fixing bracket. The outer side of a lens of the single lens reflex camera is provided with a yaw correction rotating mechanism. The pitching correction rotating shaft is provided with a pitching correction steering engine mechanism. The rolling correction rotating shaft is provided with a rolling correction steering engine mechanism. The yaw correction rotating mechanism is arranged on a yaw correction rotating steering engine at the top of the camera fixing bracket in a linkage mode. According to the three-axis aerial measurement tripod head special for the steering engine drive catapult take-off unmanned aerial vehicle, after the single lens reflex camera is installed, adjusting can be conducted in a multi-angle and multi-azimuth mode, and thus the single lens reflex camera can conduct shooting at the best angle.

Description

technical field [0001] The invention relates to a cloud platform, in particular to a three-axis aerial measurement platform dedicated to a steering gear driven ejection take-off unmanned aerial vehicle. Background technique [0002] Many aerial survey tasks require the use of imaging equipment with high imaging quality, and SLR cameras are the best choice. However, the volume and quality of the SLR camera are relatively large, and the current gimbal cannot be loaded, so the SLR camera is all fixed in the aircraft. When the UAV is operating, due to the influence of the wind, it needs to perform maneuvers such as pitch, yaw, and roll to trim the aircraft. Since the camera is fixed, when the aircraft produces a pitch angle, yaw angle or roll angle, the camera cannot always be aimed at the subject and cannot work normally. Contents of the invention [0003] In order to solve the problems of the prior art, the present invention provides a special three-axis aerial survey plat...

Claims

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Application Information

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IPC IPC(8): B64D47/08G03B17/56
CPCG03B17/56B64D47/08B64U2101/30
Inventor 耿立威
Owner 南昌白龙马航空科技有限公司
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