A measurement system according to the present embodiment includes a work tool, a sensor unit, an acquisition unit, a change unit, and a calculation unit. The work tool has a tread board with a variable width. The sensor unit is provided in the work tool. The acquisition unit acquires, from the sensor unit, time-series data on gravity center sway of a worker, in a state where the worker is standing on the tread board. The change unit reduces the width of the tread board in response to a trigger. The calculation unit calculates, from the time-series data, an evaluation value for the gravity center sway of the worker, for each width of the tread board.

A system for determining a discrete number of flexible, non-rigid workpiece items loaded onto a robotic carrier. The system includes a robotic carrier capable of traveling to multiple workstations, at least one of which is a weigh station. A loading mechanism is functional to load one or more workpieces onto the robotic carrier which weighed by the weigh station. By comparing the weight of the loaded items with a predetermined weight range of a single workpiece, the number of discrete workpieces loaded onto the robotic carrier can be determined. In addition, a method can be provided for determine position error of a mobile robot based on a detected center of gravity of the mobile robot.

The present disclosure provides an onboard object measurement system for a vehicle, such as a lift truck. The vehicle may have one or more sensors incorporated thereon, such as within one or more load handling fixtures. Control circuitry associated with the vehicle and/or the sensors is configured to receive data from the first sensor corresponding to changes in force in the first axis, receive data from the second sensor corresponding to changes in force in the second axis, correlate the changes in force along the first and second axes, and to determine one or more of a direction of motion, a thrust, or a position of a center of gravity associated with the load based on the correlation.

The invention relates to a static wheel balancer (SWB); comprising a wheel carrier (WC); wherein the wheel carrier includes at least two wheel support elements (WSE); wherein the wheel support elements (WSE) supports and establish a reference for a selected edge of a wheel when the wheel is positioned in the wheel carrier, wherein the wheel support elements (WSE) defines a wheel positioning plane (WPP); and the static wheel balancer further comprising a weight measuring arrangement (WMA) including at least one load cell (EC); wherein a weight measuring point (WMP) of the load cell (EC) is arranged to measure a partial weight of the wheel (WH) at a selected wheel edge (WE) at a given angular orientation (AO) of the wheel (WH); and wherein the weight measuring point (WMP) is arranged at a predetermined distance (PD) to at least one of the at least two-wheel support elements (WSE); and wherein the weight measuring point (WMP) forms part of one of the at least two wheel support elements (WSE); and the static wheel balancer further including a display (DP) arranged to display a measure of imbalance obtained based on partial measured weight at the weight measuring point (WMP).

The invention relates to a static wheel balancer (SWB); comprising a wheel carrier (WC); wherein the wheel carrier includes at least two wheel support elements (WSE); wherein the wheel support elements (WSE) supports and establish a reference for a selected edge of a wheel when the wheel is positioned in the wheel carrier, wherein the wheel support elements (WSE) defines a wheel positioning plane (WPP); and the static wheel balancer further comprising a weight measuring arrangement (WMA) including at least one load cell (EC); wherein a weight measuring point (WMP) of the load cell (EC) is arranged to measure a partial weight of the wheel (WH) at a selected wheel edge (WE) at a given angular orientation (AO) of the wheel (WH); and wherein the weight measuring point (WMP) is arranged at a predetermined distance (PD) to at least one of the at least two-wheel support elements (WSE); and wherein the weight measuring point (WMP) forms part of one of the at least two wheel support elements (WSE); and the static wheel balancer further including a display (DP) arranged to display a measure of imbalance obtained based on partial measured weight at the weight measuring point (WMP).

Vehicle center of gravity (CoG) height and mass estimation techniques utilize a light detection and ranging (LIDAR) sensor configured to emit light pulses and capture reflected light pulses that collectively form LIDAR point cloud data and a controller configured to estimate the CoG height and the mass of the vehicle during a steady-state operating condition of the vehicle by processing the LIDAR point cloud data to identify a ground plane, identifying a height difference between (i) a nominal distance from the LIDAR sensor to the ground plane and (ii) an estimated distance from the LIDAR sensor to the ground plane using the processed LIDAR point cloud data, estimating the vehicle CoG height as a difference between (i) a nominal vehicle CoG height and the height difference, and estimating the vehicle mass based on one of (i) vehicle CoG metrics and (ii) dampening metrics of a suspension of the vehicle.

An inner-support and gas-flotation static balancing device for a rotating ring-shaped part and a method of using the same are provided. A bottom end of an end cover is rotatably connected to a top end of a support base. One end, which is away from a working gas cavity, of the gas-flotation chamber is connected to a disc seat through a supporting column. The levelness of the gas-flotation chamber may be adjusted through the supporting column. Two axial positioning mechanisms are respectively mounted on two sides of the gas-flotation chamber in an axis direction. Gas supplied by external air supply may enter the working gas cavity, the cylindrical gas inlet channels, and the gas inlet holes through the gas supply hole, so as to form an gas film with certain bearing capacity between the working surface and the inner surface of the rotating ring-shaped part

An inner-support and gas-flotation static balancing device for a rotating ring-shaped part and a method of using the same are provided. A bottom end of an end cover is rotatably connected to a top end of a support base. One end, which is away from a working gas cavity, of the gas-flotation chamber is connected to a disc seat through a supporting column. The levelness of the gas-flotation chamber may be adjusted through the supporting column. Two axial positioning mechanisms are respectively mounted on two sides of the gas-flotation chamber in an axis direction. Gas supplied by external air supply may enter the working gas cavity, the cylindrical gas inlet channels, and the gas inlet holes through the gas supply hole, so as to form an gas film with certain bearing capacity between the working surface and the inner surface of the rotating ring-shaped part

A method is provided for producing gears to balance counteracting gravity moment and a torque equilibrator across an elevation range. The method includes assigning a value to summation of pitch radii of the first and second non-circular gears; calculating a torque for both the non-circular gears for an angle within the elevation range; calculating a first pitch radius of the first non-circular gear by the gravity moment and the torsion equilibrator; calculating a second pitch radius of the second non-circular gear from the summation; and fabricating the non-circular gears based on the first and second pitch radii.

A method is provided for producing gears to balance counteracting gravity moment and a torque equilibrator across an elevation range. The method includes assigning a value to summation of pitch radii of the first and second non-circular gears; calculating a torque for both the non-circular gears for an angle within the elevation range; calculating a first pitch radius of the first non-circular gear by the gravity moment and the torsion equilibrator; calculating a second pitch radius of the second non-circular gear from the summation; and fabricating the non-circular gears based on the first and second pitch radii.