The invention relates to a method for compacting coil windings (52) which are wound on a tooth core (10) of a stator segment (1), wherein an insulation layer (36) is disposed between coil windings and the tooth core, and the tooth core (10) has, between a yoke region (14) and a tooth region (12) in a tooth height direction (ZH), a tooth core neck (16) and has, between the yoke region (14) and the tooth head (12) in a tooth width direction (ZB), groove halves (30, 30) running in a tooth length direction (ZL), in which groove halves the coil windings (52) lie, and wherein according to the invention the coil windings (52) are compressed in the tooth width direction (ZB) and in the tooth length direction (ZL) by at least four pressing jaws (84, 90, 90, 100, 110, 112, 112). The invention also relates to a device, wherein according to the invention the device has, for compressing the coil windings (52), coil contour jaws (110, 110) which can be moved in a tooth width direction (ZB) and coil head jaws (90, 90) which can be moved in a tooth length direction (ZL). The invention further relates to a stator segment (1) compacted by means of the method, the stator segment having a distance space between each of a plurality of uninsulated surfaces of the tooth core (10) in the groove base gap and/or at the edge of the pole surface (20) of the tooth head (12) and a coil (50) wound around the tooth core (10).

Systems and methods for facilitating aerial vehicle services are provided. A service entity system can obtain multi-modal transportation services data indicative of a plurality of anticipated aerial transportation service. The service entity system can obtain vehicle attributes associated vehicle(s) of an aerial vehicle provider and determine an expected performance of the vehicle(s) based on the vehicle attributes and the anticipated aerial transportation services. The service entity system can generate an aerial vehicle service request that requests access to the vehicle(s) for providing aerial transportation services for the service entity based on the expected performance of the vehicle(s). A vehicle provider system can obtain a number of different aerial vehicle service requests from a number of different service entities. The vehicle provider system can select portions of the different aerial vehicle service requests to accept and provide access to vehicle(s) of the vehicle provider based on the selected portions.

A system for using a space integration sequencer system that coordinates timing of aircraft operations including arrivals, departures, and enroute flights with current and future aircraft operations. The system includes an overall system input, an overall system logic, and an overall system output. The overall system input includes a plurality of vehicle telemetry and a plurality of regulatory data. The overall system logic includes a pathway identifier, a first pathway intersection, an algorithm, and a second pathway intersection. The overall system output includes a pathway generator and a pathway reroute. The overall system includes a camera-based sensor system includes a Pan-Tilt-Zoom camera, an edge computer, a backup battery, and an optional solar power source and a Light Detection and Ranging system that includes a plurality of lasers, a scanner, a Global Positioning System, and an Inertial Measurement Unit.

A system for using a space integration sequencer system that coordinates timing of aircraft operations including arrivals, departures, and enroute flights with current and future aircraft operations. The system includes an overall system input, an overall system logic, and an overall system output. The overall system input includes a plurality of vehicle telemetry and a plurality of regulatory data. The overall system logic includes a pathway identifier, a first pathway intersection, an algorithm, and a second pathway intersection. The overall system output includes a pathway generator and a pathway reroute. The overall system includes a camera-based sensor system includes a Pan-Tilt-Zoom camera, an edge computer, a backup battery, and an optional solar power source and a Light Detection and Ranging system that includes a plurality of lasers, a scanner, a Global Positioning System, and an Inertial Measurement Unit.

In accordance with an aspect of the present disclosure, there is provided a method for dividing a corridor of UAM (urban air mobility) into a plurality of regions by a corridor dividing device, the method comprising, acquiring information on a flight operation area of the UAM, and dividing a corridor defined in the flight operation area into a plurality of regions based on the information on the flight operation area, wherein the information on the flight operation area includes at least one of information on a region of interest in the flight operation area and information on an event which occurs in the flight operation area.

In accordance with an aspect of the present disclosure, there is provided a method for dividing a corridor of UAM (urban air mobility) into a plurality of regions by a corridor dividing device, the method comprising, acquiring information on a flight operation area of the UAM, and dividing a corridor defined in the flight operation area into a plurality of regions based on the information on the flight operation area, wherein the information on the flight operation area includes at least one of information on a region of interest in the flight operation area and information on an event which occurs in the flight operation area.

Generally discussed herein are systems, apparatuses, and methods for simulating an airspace including a method that receives a plurality of flight intent data inputs from a plurality of sources including service suppliers of unmanned aircraft systems (UAS) traffic management (UTM), advanced air mobility (AAM) and conventional air traffic management (ATM). The plurality of flight intent data inputs include, UTM flight intent volumes, UTM flight intent trajectories, conventional flight plans, conventional flight trajectories and an airspace design configuration. The method includes generating a center line route corresponding to each of the plurality of flight intent data inputs; generating a flight volume for each the plurality of flight intent data inputs; generating a four-dimensional trajectory based upon the center line route and the flight volume; and verifying the four-dimensional trajectory against constraints and potential conflicts.

A system comprises a processor onboard a vehicle, surveillance sensors, and a DAA module that receives sensor measurement tracks and includes a tracking system that tracks objects in an environment around the vehicle. The tracking system comprises a data association module that includes a track-to-track function that outputs main solution and sub-solution tracks with track information. An integrity module communicates with the DAA module and comprises a track integrity system in communication with the data association module and operative to provide integrity checks. The track integrity system compares, selects, and outputs a main solution track or sub-solution tracks based on correlated tracks provided by the track-to-track function and solution separation; sends a track solution that passes integrity tests to a prune function, and sends tracks that fail to pass integrity tests to the data association module; and assures the integrity of tracks correlated and estimated by the tracking system.

A system comprises a processor onboard a vehicle, surveillance sensors, and a DAA module that receives sensor measurement tracks and includes a tracking system that tracks objects in an environment around the vehicle. The tracking system comprises a data association module that includes a track-to-track function that outputs main solution and sub-solution tracks with track information. An integrity module communicates with the DAA module and comprises a track integrity system in communication with the data association module and operative to provide integrity checks. The track integrity system compares, selects, and outputs a main solution track or sub-solution tracks based on correlated tracks provided by the track-to-track function and solution separation; sends a track solution that passes integrity tests to a prune function, and sends tracks that fail to pass integrity tests to the data association module; and assures the integrity of tracks correlated and estimated by the tracking system.

A system for using a space integration sequencer system that coordinates timing of aircraft operations including arrivals, departures, and enroute flights with current and future aircraft operations. The system includes an overall system input, an overall system logic, and an overall system output. The overall system input includes a plurality of vehicle telemetry and a plurality of regulatory data. The overall system logic includes a pathway identifier, a first pathway intersection, an algorithm, and a second pathway intersection. The overall system output includes a pathway generator and a pathway reroute. The overall system includes a camera-based sensor system includes a Pan-Tilt-Zoom camera, an edge computer, a backup battery, and an optional solar power source and a Light Detection and Ranging system that includes a plurality of lasers, a scanner, a Global Positioning System, and an Inertial Measurement Unit.