Triaxial orthographic nacelle of unmanned aerial vehicle
A technology of unmanned aerial vehicles and pods, applied in the field of three-axis ortho-firing pods of unmanned aerial vehicles, can solve problems such as unfavorable promotion and use, high price, etc., and achieve enhanced detection and identification capabilities, convenient maintenance or replacement, and compact structure. Effect
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2013-11-20
- Estimated Expiration
- Not applicable · inactive patent
Smart Images
Figure 1 Figure 2 Figure 3
Abstract
Description
technical field
[0001] The invention relates to a three-axis orthographic pod for an unmanned aerial vehicle, which belongs to the technical field of photoelectric equipment in aircraft and aviation technology. Background technique
[0002] In the process of remote sensing aerial photography, remote sensing instruments are required to be as stable as possible, especially aerial photogrammetry, which requires that the heading overlap rate and side overlap rate are both greater than a certain value, which requires the camera to keep approximately vertical to the ground.
[0003] When the attitude angle changes greatly, the aerial photography images tend to have too low or no overlap, resulting in aerial photography loopholes, resulting in the unusable route image data with loopholes, and the aerial photography needs to be re-used.
[0004] Therefore, it is necessary to use a stable platform to compensate the attitude change of the flying platform to ensure the quality of camer...
Examples
Embodiment Construction
[0020] The present invention will be described in further detail below in conjunction with the accompanying drawings.
[0021] refer to figure 1 As shown, the present invention discloses a three-axis orthographic pod for an unmanned aerial vehicle, which is composed of a pitch assembly 1, a roll assembly 2, a heading assembly 3 and a circuit board assembly 4. The pitch assembly 1, roll assembly 2 , and the course component 3 and the circuit board component 4 realize information transmission through connecting cables.
[0022] Such as figure 2 , image 3 As shown, the pitch axis group 1 includes an outer shell 108 connected to the aircraft pylon and a pitch support 101 connected to the outer shell 108, and the first pitch side plate 103 and the second pitch side plate 105 are fixed on the pitch support 101 And the attitude measurement system 107, the first pitch side plate 103 is provided with a pitch motor group 102, the second pitch side plate 105 is provided with a resol...