Flight ranging system and correction method
A technology of ranging system and correction method, applied in the field of time-of-flight ranging system and correction that can avoid offset, and can solve problems such as interval-time interval and the like
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2019-08-23
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Abstract
Description
technical field
[0001] The present application relates to a time-of-flight ranging system and a calibration method, and in particular, to a time-of-flight ranging system and a calibration method that can avoid offsets. Background technique
[0002] With the rapid development of science and technology, the acquisition of three-dimensional information of objects has broad application prospects in many application fields, such as production automation, human-computer interaction, medical diagnosis, reverse engineering, digital modeling, etc. Among them, the structured light three-dimensional measurement method, as a non-contact three-dimensional information acquisition technology, has been widely used because of its advantages of simple implementation, high speed and high precision.
[0003] Time of Flight (ToF) ranging method is a commonly used three-dimensional depth measurement method. However, the existing time-of-flight ranging system has many non-idealities. For example,...
Examples
Embodiment Construction
[0021] In order to make the purpose, technical solutions and advantages of the present application more clearly understood, the present application will be described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application, but not to limit the present application.
[0022] Please refer to figure 1 , figure 1 It is a schematic diagram of the time-of-flight ranging system 10 according to the embodiment of the present application. The time-of-flight ranging system 10 includes a delay unit 12 , a light-emitting unit 13 , a photosensitive pixel array 14 , a storage unit 16 and a control unit 18 . In the calibration stage of the time-of-flight ranging system 10, the reflector 11 is set at a known fixed distance GD from the time-of-flight ranging system 10, and the light-emitting unit 13 emits light toward the reflector 11 to sense the ...