The present invention relates to the field of radar detection. Provided are a detection method and a detection apparatus. The method comprises: emitting a first waveform signal to a target to undergo detection, and receiving a second waveform signal reflected by the target on the basis of the first waveform signal, the second waveform signal carrying spatial modulation information; generating, on the basis of the second waveform signal, a detection signal corresponding to the spatial modulation information, and obtaining a signal flight time carried on the detection signal; and determining distance data of the target on the basis of multiple pieces of the spatial modulation information and signal flight times corresponding thereto.

The present invention relates to the field of radar detection. Provided are a detection method and a detection apparatus. The method comprises: emitting a first waveform signal to a target to undergo detection, and receiving a second waveform signal reflected by the target on the basis of the first waveform signal, the second waveform signal carrying spatial modulation information; generating, on the basis of the second waveform signal, a detection signal corresponding to the spatial modulation information, and obtaining a signal flight time carried on the detection signal; and determining distance data of the target on the basis of multiple pieces of the spatial modulation information and signal flight times corresponding thereto.

A method for analyzing backscatter histogram data in an optical pulse runtime method, including the steps of receiving backscatter histogram data; and analyzing the received backscatter histogram data.

A method for analyzing backscatter histogram data in an optical pulse runtime method, including the steps of receiving backscatter histogram data; and analyzing the received backscatter histogram data.

Provided is a phase difference calculation device including a first light amount acquisition unit that acquires a first light amount of reflected light of light applied in a first time window and received in the first time window and a second light amount of the reflected light received in a second time window, a time window shift control unit that shifts the first and second time windows and a third time window in the negative direction of the time axis to set fourth, fifth, and sixth time windows, and shifts the fourth, fifth, and sixth time windows in the negative direction of the time axis until no reflected light is received in the fourth time window, a second light amount acquisition unit that acquires a third light amount of the reflected light received in the sixth time window, and a phase difference calculation unit that calculates a phase difference between the light and the reflected light on the basis of a first corrected light amount obtained by adding the third light amount to the first light amount and a second corrected light amount obtained by subtracting the third light amount from the second light amount.

Disclosed herein are system and method embodiments to implement a scout pulse LiDAR. An embodiment operates by emitting a leading sequence of two or more discrete pulses with a constant timing offset and large intensity ratio. These leading pulses are each called a ‘scout pulse’ because they scout ahead of the primary pulse to detect high intensity targets, which would otherwise saturate the detector. In the simplest configuration, there are only two pulses, one primary pulse (lagging, high power/intensity) and one scout pulse (leading, low power/intensity). In more complex configurations, there may be any number of multiple scout pulses, each with a unique time delay and intensity. In any configuration, the signals are emitted in order of ascending intensity, with the lowest intensity signal in front (first), and the highest intensity signal in the back (last) within the pulse train.

An operating method for a LIDAR system that is operable by pulse sequence encoding and designed with a SPAD-based detector element, in which a down time of the SPAD-based detector element is detected, and in the transmission mode of the LiDAR system, a minimum time interval of transmission pulses of primary light to be transmitted in direct chronological succession is dimensioned in such a way that the minimum time interval at least approximately corresponds to the down time.

An operating method for a LIDAR system that is operable by pulse sequence encoding and designed with a SPAD-based detector element, in which a down time of the SPAD-based detector element is detected, and in the transmission mode of the LiDAR system, a minimum time interval of transmission pulses of primary light to be transmitted in direct chronological succession is dimensioned in such a way that the minimum time interval at least approximately corresponds to the down time.

A LIDAR noise removal apparatus and a LIDAR noise removal method thereof are provided. The apparatus includes a LIDAR detection information processor that processes LIDAR detection information received from a LIDAR of a vehicle. A sun position acquirer acquires an azimuth angle and elevation angle of the sun relative to a traveling direction of the vehicle. An ROI selector selects an ROI corresponding to the sun from a front image of the vehicle based on the azimuth angle and elevation angle and compares a brightness of the selected ROI with a threshold value. A noise region selector selects a noise region corresponding to the ROI from the LIDAR detection information based on the azimuth angle and elevation angle when the brightness of the ROI exceeds the threshold value, and a noise remover removes noise points in the selected noise region.

A time of flight (TOF) measurement method and apparatus are provided, including a controller, a time to digital converter, a pulse transmitter, and a pulse receiver. The controller is configured to control, in a working period according to a predetermined transmit rule, the pulse transmitter to sequentially send M transmit pulses. The pulse receiver is configured to receive N feedback pulses in the working period. The time to digital converter is configured to obtain time of flight information corresponding to the N feedback pulses. The controller is further configured to obtain a target time of flight based on the time of flight information corresponding to the N feedback pulses, and obtain a target distance based on the target time of flight.