Abstract: An apparatus for controlling a tilt rotor is provided. The apparatus includes a thrust command generator configured to generate a first collective pitch angle based on a throttle command, a rotation speed compensator configured to generate a compensation value based on a rotation speed of the motor, a compensation weight generator configured to generate weight values according to a flight speed, a collective pitch angle command generator configured to generate a collective pitch angle adjustment command of the rotor blade of the motor, based on the first collective pitch angle and a first compensation value being obtained by multiplying the compensation value by a preset conversion ratio and a first weight value, and a motor controller configured to generate a motor control command based on a second compensation value being obtained by multiplying the compensation value by a second weight value and the first collective pitch angle.

Abstract: Provided is a vertical take-off/landing aircraft controlling a tilt angle of a main rotor, based on a vertical posture control signal during low-speed flight, wherein, when an aircraft steering signal including a vertical posture control signal for changing the pitch posture angle of the vertical take-off/landing aircraft by a first pitch posture angle is obtained, a flight controller determines a tilt angle of the main rotor with reference to the first pitch posture angle and generates a tilt angle control signal for the main rotor based on the determined tilt angle.

Abstract: The present invention relates to a control input device applicable to an eVTOL aircraft, which is an electric-powered vertical take-off and landing aircraft, and more particularly, to an aircraft control input device that may replace a cyclic control stick, a tail rotor control pedal, and a collective control stick used for flight control of a conventional aircraft, which is simpler in configuration and easier to operate than conventional control devices and may improve pilot convenience and stability of flight operation through simple and accurate flight manipulation, and a command input method using the same.

Abstract: Provided is a system for controlling an RPM of a propeller and a rotor of a flight vehicle having multiple power units including: a collective pitch angle command generating unit generating a collective pitch angle command upon receiving a thrust control command from a pilot or an automatic controller; a disturbance factor compensating unit for generating an RPM compensation electronic speed control (ESC) command for compensating for an RPM error, and an electronic speed adjustment command generating unit generating a final ESC command upon receiving a collective command input or derived in the process of generating the collective pitch angle command by the collective pitch angle command generating unit and the RPM compensation ESC command generated by the disturbance factor compensating unit. RPMs of motors of a flight vehicle having a plurality of propellers and rotors may be maintained to be the same.

Abstract: Disclosed embodiments provide systems and methods related to monitoring logistics. A method for monitoring logistics comprises capturing attendance data and timekeeping data for a first plurality of workers from a first management system, data identifying work performed by a second plurality of workers, the data comprising a location of performed work, an associated scan event, or clock-in information associated with each of a second plurality of workers, from a second management system, and work data related to a third plurality of workers from a third management system. The method further comprises consolidating the captured data on workers having corresponding data in one of the captured sets of data, receiving a request from a user device, for a visualization including analysis of the consolidated data, and providing a visualization to the user device, wherein the visualization is generated by analyzing the consolidated data.

Abstract: Disclosed embodiments provide systems and methods related to monitoring logistics. A method for monitoring logistics comprises capturing attendance data and timekeeping data for a first plurality of workers from a first management system, data identifying work performed by a second plurality of workers, the data comprising a location of performed work, an associated scan event, or clock-in information associated with each of a second plurality of workers, from a second management system, and work data related to a third plurality of workers from a third management system. The method further comprises consolidating the captured data on workers having corresponding data in one of the captured sets of data, receiving a request from a user device, for a visualization including analysis of the consolidated data, and providing a visualization to the user device, wherein the visualization is generated by analyzing the consolidated data.

Abstract: Disclosed embodiments provide systems and methods related to monitoring logistics. A method for monitoring logistics comprises capturing attendance data and timekeeping data for a first plurality of workers from a first management system, data identifying work performed by a second plurality of workers, the data comprising a location of performed work, an associated scan event, or clock-in information associated with each of a second plurality of workers, from a second management system, and work data related to a third plurality of workers from a third management system. The method further comprises consolidating the captured data on workers having corresponding data in one of the captured sets of data, receiving a request from a user device, for a visualization including analysis of the consolidated data, and providing a visualization to the user device, wherein the visualization is generated by analyzing the consolidated data.

Abstract: Embodiments of the present disclosure include computer-implemented systems and methods for package delivery. The method may comprise receiving a customer order, generating an order identifier, associating each item of the customer order with the order identifier, and determining an intended delivery destination for each item. The method may further comprise causing the user-device to display a first indication to sort each item based on the storage space associated with the intended delivery destination, display a second indication to sort the sorted each item based on the delivery route, display a third indication to place the sorted each item into a container, without regard to a status of the other items of the customer order, and display a fourth indication to deliver the placed items of the plurality of items to the intended delivery destination, without regard to the status of the other items of the customer order.

Abstract: Disclosed embodiments provide systems and methods related to monitoring logistics. A method for monitoring logistics comprises capturing attendance data and timekeeping data for a first plurality of workers from a first management system, data identifying work performed by a second plurality of workers, the data comprising a location of performed work, an associated scan event, or clock-in information associated with each of a second plurality of workers, from a second management system, and work data related to a third plurality of workers from a third management system. The method further comprises consolidating the captured data on workers having corresponding data in one of the captured sets of data, receiving a request from a user device, for a visualization including analysis of the consolidated data, and providing a visualization to the user device, wherein the visualization is generated by analyzing the consolidated data.

Abstract: Provided is a vertical take-off/landing aircraft controlling a tilt angle of a main rotor, based on a vertical posture control signal during low-speed flight, wherein, when an aircraft steering signal including a vertical posture control signal for changing the pitch posture angle of the vertical take-off/landing aircraft by a first pitch posture angle is obtained, a flight controller determines a tilt angle of the main rotor with reference to the first pitch posture angle and generates a tilt angle control signal for the main rotor based on the determined tilt angle.