Aviation different-speed image motion compensation circuit, CCD driving circuit and driving method

A technology of image movement compensation and driving circuit, which is applied in the field of aerial image processing to ensure the consistency of timing and improve the effect.
CN110149488AActive Publication Date: 2019-08-20CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
Publication Date
2019-08-20

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Abstract

The invention is applicable to the technical field of displays, and provides an aviation different-speed image motion compensation circuit, which comprises a main time sequence generator, used for generate driving time sequence required by a CCD; a different-speed image motion time sequence controller, used for forwarding the driving time sequence generated by the main time sequence generator andgenerating an image motion compensation driving time sequence during different-speed image motion compensation; and a driving circuit used for amplifying and translating the driving time sequence output by the different-speed image motion time sequence controller so as to drive the CCD. The main time sequence generator is added to the aviation different-speed image motion compensation circuit, andthe main time sequence generator uniformly calculates various compensation parameters during different-speed image motion compensation, so that the time sequence consistency during different-speed image motion compensation is effectively ensured, and the effect of different-speed image motion compensation is better improved.
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Description

technical field

[0001] The invention belongs to the technical field of aerial image processing, and in particular relates to an aerial image motion compensation circuit at different speeds, a CCD driving circuit and a driving method. Background technique

[0002] In the reconnaissance process, the reconnaissance plane often needs to fly at high speed and low altitude (high speed and height ratio) in order to avoid radar surveillance. At this time, image motion blur will inevitably appear in aerial imaging. The formation of image motion blur is closely related to the flight attitude of the carrier aircraft. Different parameters such as the flight speed, altitude, roll angle, yaw angle, and pitch angle of the carrier aircraft will produce different image motion forms. Among them, when the carrier aircraft is flying sideways or the lens is pitched to the side, the aerial camera on the carrier aircraft will be in a squint working state. At this time, different positions on the ...

Claims

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