A method of time of flight sensing. The method comprises using an emitter to emit pulses of radiation and using an array of photo-detectors to detect radiation reflected from an object. For a given group of photo-detectors of the array, the method determines based upon measured times of flight of the radiation, whether to use a first mode of operation in which outputs from individual photo-detectors of the group are combined together or to use a second mode of operation in which outputs from individual photo-detectors are processed separately. The array of photo-detectors comprises a plurality of groups of photo-detectors. One or more groups of photo-detectors operate in the first mode whilst in parallel one or more groups of photo-detectors operate in the second mode.

A laser ranging device and a robot. The laser ranging device comprises an emitting unit and a receiving unit. The emitting unit comprises an emitter configured to emit a laser pulse to a target object that is to be ranged, and an emitting lens configured for the laser pulse to pass through. The receiving unit comprises a photodetector configured to receive a reflected laser pulse by the target object, and a receiving lens configured for the reflected laser pulse to pass through. The photodetector is encapsulated in an encapsulation module, the encapsulation module is disposed aft of and faces the receiving lens, and a side surface of the encapsulation module facing the receiving lens is constructed as an extinction surface.

A laser ranging device and a robot. The laser ranging device comprises an emitting unit and a receiving unit. The emitting unit comprises an emitter configured to emit a laser pulse to a target object that is to be ranged, and an emitting lens configured for the laser pulse to pass through. The receiving unit comprises a photodetector configured to receive a reflected laser pulse by the target object, and a receiving lens configured for the reflected laser pulse to pass through. The photodetector is encapsulated in an encapsulation module, the encapsulation module is disposed aft of and faces the receiving lens, and a side surface of the encapsulation module facing the receiving lens is constructed as an extinction surface.

A control unit 15 of an in-vehicle device 1 configured to acquire, from landmark data LD that is map data including position information of one or more features, plural pieces of position information of a feature which is drawn on a road surface and which exists at or around a vehicle. Then, the control unit 15 is configured to calculate a normal vector of an approximate plane calculated based on the acquired plural pieces of the position information. Then, the control unit 15 is configured to calculate at least one of a pitch angle or a roll angle of the vehicle based on the orientation of the vehicle and the normal vector.

A rangefinder includes a light emitting part, a light receiving part, a calculating part that calculates the distance from a reflective object, and a control part. The calculating part has a received light intensity determining part, a peak detecting part, and a distance calculating part, and a distance determining part. The control part controls at least one of the intensity of the pulsed light, the sensitivity of the light receiving part to received light, and a position of the region of interest so that a first received light intensity is obtained as the received light intensity of each of the plurality of times of flight at least once, and a second received light intensity having a higher S/N ratio is obtained as the received light intensity of each of the plurality of times of flight at least once. The distance determining part determines the measurement target distance by using the first distance based on the first received light intensity and the second distance based on the second received light intensity.

A rangefinder includes a light emitting part, a light receiving part, a calculating part that calculates the distance from a reflective object, and a control part. The calculating part has a received light intensity determining part, a peak detecting part, and a distance calculating part, and a distance determining part. The control part controls at least one of the intensity of the pulsed light, the sensitivity of the light receiving part to received light, and a position of the region of interest so that a first received light intensity is obtained as the received light intensity of each of the plurality of times of flight at least once, and a second received light intensity having a higher S/N ratio is obtained as the received light intensity of each of the plurality of times of flight at least once. The distance determining part determines the measurement target distance by using the first distance based on the first received light intensity and the second distance based on the second received light intensity.

Methods and systems for performing multiple pulse LIDAR measurements are presented herein. In one aspect, each LIDAR measurement beam illuminates a location in a three dimensional environment with a sequence of multiple pulses of illumination light. Light reflected from the location is detected by a photosensitive detector of the LIDAR system during a measurement window having a duration that is greater than or equal to the time of flight of light from the LIDAR system out to the programmed range of the LIDAR system, and back. The pulses in a measurement pulse sequence can vary in magnitude and duration. Furthermore, the delay between pulses and the number of pulses in each measurement pulse sequence can also be varied. In some embodiments, the multi-pulse illumination beam is encoded and the return measurement pulse sequence is decoded to distinguish the measurement pulse sequence from exogenous signals.

Methods and systems for performing multiple pulse LIDAR measurements are presented herein. In one aspect, each LIDAR measurement beam illuminates a location in a three dimensional environment with a sequence of multiple pulses of illumination light. Light reflected from the location is detected by a photosensitive detector of the LIDAR system during a measurement window having a duration that is greater than or equal to the time of flight of light from the LIDAR system out to the programmed range of the LIDAR system, and back. The pulses in a measurement pulse sequence can vary in magnitude and duration. Furthermore, the delay between pulses and the number of pulses in each measurement pulse sequence can also be varied. In some embodiments, the multi-pulse illumination beam is encoded and the return measurement pulse sequence is decoded to distinguish the measurement pulse sequence from exogenous signals.

The present invention relates to a light detection and ranging (LiDAR) system. The LiDAR system may include a transceiver configured to generate pieces of light having different wavelengths and receive pieces of reflected light having different wavelengths reflected from a target, a beam splitter configured to divide the pieces of light having the different wavelengths into long-wavelength light having a relatively long wavelength and short-wavelength light having a relatively short wavelength, and a scan mirror configured to transmit the long-wavelength light and the short-wavelength light, which are divided by the beam splitter, to an outside and allow reflected light of the long-wavelength light and reflected light of the short-wavelength light to be incident on the transceiver through the beam splitter.

A total station or a theodolite includes scanning functionality for optical surveying of an environment, in which the total station or the theodolite is configured such that direction-dependent active acquisition regions of the receiver are defined depending on the transmission direction of the transmitted radiation to adapt the receiver surface mechanically and/or electronically to a varying imaging position of the received radiation on the overall detector surface.