Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

168 results about "Noise correction" patented technology

Signal processing device and method

The present invention provides a signal processing device which, even when a defective pixel exists in the VOPB area B, can detect column noise accurately, and can carry out column noise correction. The signal processing device includes a solid-state image pickup element having a pixel part including an effective pixel area to be irradiated with light, and a vertical light-shielded pixel area where irradiation of light is shielded, a vertical scanning circuit, a horizontal scanning circuit, and an output circuit, a clamp section which clamps, to a predetermined reference value, black level values of pixel signals from the vertical light-shielded pixel area and effective pixel area, a threshold determination section which determines a threshold value, based on the predetermined reference value, a determination section which determines whether or not pixel signals from the vertical light-shielded pixel area that have the black level value clamped to the reference value by the clamp section exceed the threshold value determined by the threshold determination section, a defective pixel detector which detects a defective pixel among pixels arranged in the vertical light-shielded pixel area, and a signal processor which performs a predetermined signal processing on pixel signals from the vertical light-shielded pixel area that have a black level value clamped to the reference value by the clamp section.
Owner:SONY CORP

Image-pickup device and signal processing method for noise correction

The present invention provides an image pickup device that can accurately adjust the black level value of the effective pixel area while correcting column noise contained in pixel signals of the effective pixel area. The image pickup device includes a solid-state image pickup element having a pixel part including an effective pixel area to be irradiated with light, a vertical light-shielded pixel area and a horizontal light-shielded pixel area where irradiation of light is shielded, a vertical scanning circuit, a horizontal scanning circuit, and an output circuit, a light-shielding section which shuts off light irradiated on the effective pixel area, a black level value detector which detects black level values of the vertical light-shielded pixel area, the horizontal light-shielded pixel area, and the effective pixel area shielded from light by the light-shielding section, based on pixel signals outputted from the output circuit of the solid state image pickup element, a comparator which compares the black level values, a noise component detector which detects a noise component, a noise corrector which corrects noise generated in the effective pixel area, based on the noise component detected by the noise component detector, and a controller which controls the noise component detector and the noise corrector, based on a comparison result of the comparator.
Owner:SONY CORP

Transition Reynolds number acquisition method under condition of flight

ActiveCN108287054AGuaranteed Transition Reynolds NumberLow costAerodynamic testingStability theoryCurve fitting
The invention relates to a transition Reynolds number acquisition method under the condition of flight. Firstly, shrinkage model test meeting the test similarity criterion is carried out in a ground wind tunnel to obtain a transition Reynolds number under the ground simulation condition; secondly, air-ground difference analysis is conducted, and the change data of the transition Reynolds number with an amplification factor N at different wall temperatures is given based on the flow stability theory; thirdly, the change law of the reference value of the transition Reynolds number with the walltemperature is obtained, and a wall temperature correction formula is obtained through curve fitting; fourthly, the change data of the transition Reynolds number with the amplification factor N afternormalization is obtained, and a noise correction formula is obtained; and finally, a unified extrapolation formula is formed, and a transition Reynolds number under the condition of flight is obtained through extrapolation based on a ground transition Reynolds number. The method has the advantage as follows: the transition test data is highly reliable and accurate, the cost of the method is muchlower than that of a method in which an association formula is obtained through test data fitting; and the data obtained by the stability theory is more regular, and the function relation is more accurate.
Owner:CHINA ACAD OF AEROSPACE AERODYNAMICS
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products