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Aerospace three linear array CCD camera vision main point on-rail monitoring method

A three-line array and camera technology, applied in the field of aerospace satellite photogrammetry, can solve the problems of inability to perform real-time monitoring, unsuitable for measurement requirements, complicated processes, etc., and achieve the effects of reducing laser beam drift, easy operation, and improving stability.

Inactive Publication Date: 2011-04-27
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH +1
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Problems solved by technology

However, this method is very complicated and time-consuming. It is suitable for regular inspection of the accuracy of the principal point of view of the camera, and cannot be used for real-time monitoring. It is not suitable for global satellite photogrammetry without ground control points.

Method used

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  • Aerospace three linear array CCD camera vision main point on-rail monitoring method
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  • Aerospace three linear array CCD camera vision main point on-rail monitoring method

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Embodiment Construction

[0018] Such as figure 1 Shown is a schematic diagram of the principle of the monitoring method of the present invention. To monitor the principal point of view of the camera using the method of the present invention, a laser emitting device needs to be arranged on the camera lens, and two receiving phases should be arranged on the line array CCD. The laser emitting device must be rigidly fixed to the camera lens, and the two receiving phases must be rigidly fixed to the linear array CCD.

[0019] The structure of the laser emitting device is as follows figure 2 As shown, it includes a laser light source 1, a fiber coupler 3 and two laser collimators 4. The laser light emitted by the laser light source 1 is sent to the fiber coupler 3 through the fiber 2, and the fiber coupler 3 splits the incoming laser light into two paths. Afterwards, they are respectively sent to two laser collimators 4 to obtain collimated lasers and then output. In order to meet the requirements of th...

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Abstract

The invention relates to an aerospace three linear array CCD camera vision main point on-rail monitoring method, wherein a laser emitting device is rigidly fixed on a camera lens; and a first area array CCD and a second area array CCD are symmetrically and rigidly fixed on both sides of the linear array CCD. The position of camera lens is adjusted so that the main optical axis of the camera lens passes through the center of the linear array CCD; simultaneously, the position of laser emitting device is adjusted so that two ways of lasers output by the laser emitting device are symmetrically incident into the camera lens relative to the main optical axis and respectively transmitted to the first area array CCD and the second area array CCD by the camera lens. The variation volume of camera vision main point can be determined by the displacement change of the imaging point of laser beam on the first area array CCD in horizontal and vertical directions and the displacement change of imaging point of laser beam on the second area array CCD in horizontal and vertical directions. The invention uses non-contact measuring method without affecting the normal work of camera, thereby realizing the nano-scale high-precision measurement of vision main point change.

Description

technical field [0001] The invention belongs to the technical field of aerospace satellite photogrammetry, and relates to an on-orbit monitoring method for the change of the principal point of view of an aerospace three-line array CCD camera. Background technique [0002] The principal point of view of the aerospace three-line array CCD camera is the intersection point of the main optical axis of the camera lens and the linear array CCD. It is an important internal parameter of the aerospace camera and directly affects the accuracy of the photogrammetry of the aerospace satellite. At present, the position of the apparent principal point of the three-line array CCD camera in the spaceflight can be determined by precise verification in the ground laboratory before launch, but after the satellite is launched into the sky, due to the influence of weightlessness and temperature changes during the satellite’s in-orbit flight, it will cause spaceflight The main point of view of the...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C11/00
Inventor 高卫军郎晓萍宗云花刘力双段维宏吕勇
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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