Abstract: Calibrating an unstable sensor of a mobile device. Systems and methods for calibrating a sensor of a mobile device determine a first estimated position of the mobile device without using any measurement from the sensor of the mobile device, generate a second estimated position of the mobile device using a measurement from the sensor, estimate a sensor error of the sensor using the first estimated position and the second estimated position, and use the sensor error to determine a calibration value for adjusting one or more measurements from the sensor.

Abstract: Systems and methods directed to improvements in the presentation of CAVS procedures on an aircraft display system over what is conventionally available are provided. The provided systems and methods employ a vertical situation display (VSD), thereby presenting additional relevant visual approach information, such as a vertical distance between the ownship and the target aircraft, descent rates of the ownship and the target and an alerting function for the user-selected CAVS range. The provided systems and methods also capably receive and process user selections of target aircraft from both the lateral display and the VSD.

Abstract: A system for providing integrated detection and deterrence against an unmanned vehicle including but not limited to aerial technology unmanned systems using a detection element, a tracking element, an identification element and an interdiction or deterrent element. Elements contain sensors that observe real time quantifiable data regarding the object of interest to create an assessment of risk or threat to a protected area of interest. This assessment may be based e.g., on data mining of internal and external data sources. The deterrent element selects from a variable menu of possible deterrent actions. Though designed for autonomous action, a Human in the Loop may override the automated system solutions.

Abstract: Methods and systems for controlling the flight of aircraft are disclosed. An example system includes a flight management computer to receive a first time of arrival at a first target waypoint of an aircraft and a second time of arrival at a second target waypoint, determine a first set of cruise speed and descent speed pairs corresponding to the first time, the first set satisfying the first time, determine a second set of cruise speed and descent speed pairs corresponding to the second time, the second set satisfying the second time, select a cruise speed and descent speed pair from the first set or the second set, determine an aircraft trajectory that satisfies the selected cruise speed and descent speed pair, and cause at least one of: 1) the aircraft to travel along the aircraft trajectory or 2) the aircraft trajectory to be displayed.

Abstract: A collision warning method includes receiving a collision risk indication from a traffic collision avoidance system of an aircraft, receiving a preset altitude, comparing the preset altitude and an altitude associated with the collision risk indication, and providing a warning in the aircraft when the preset altitude and the altitude associated with the collision risk are within a threshold.

Abstract: Example systems and methods for controlling a flight of an aircraft subjected to a required time of arrival constraint at a target waypoint and to an additional flight criterion are disclosed herein. An example method includes calculating combinations of cruise speed and descent speed for estimated times of arrival (ETAs) at the target waypoint and determining a subset of the combinations that introduce substantially a same amount of time change in the ETA when changing the corresponding cruise speed to a cruise speed limit as when changing the corresponding descent speed to a descent speed limit. The example method also includes selecting a combination of the subset of the combinations having an ETA substantially equal to the RTA and modifying at least one of a cruise speed or a descent speed of the aircraft based on the selected combination.

Abstract: A client terminal and a server system having a plurality of processing units processing game applications are connected to each other via a network. In a game system was a cloud computing system, the server system makes the client terminal wait for a start of processing of an application when there is no processing unit assignable to the client terminal. The client terminal processes another application locally in a state of waiting for the start of the processing of the application in the server system.

Abstract: A system and method are provided for graphically displaying airspace data including speed restrictions on an aircraft display. The system comprises an avionics display system coupled to a processor that is configured to retrieve airspace data from a database, display the aircraft data on the display, and display a visual representation of the airspace. Then the processor may alter the format of the visual representation of the airspace to a second visual representation, if the airspace data meets predetermined criteria.

Abstract: Methods and systems for guiding an aircraft are disclosed herein. An example method includes determining, via a processor, a difference between an estimated time of arrival and a required time of arrival of an aircraft. The example method also includes determining if the difference exceeds a threshold time. The example method further includes determining a deviation between a predicted four-dimensional flight trajectory of the aircraft and a measured four-dimensional flight trajectory of the aircraft during flight if the difference does not exceed the threshold time. The example method also includes generating a speed command to reduce the deviation and updating a flight plan of the aircraft based on the speed command.

Abstract: A system and method to improve efficiency in aircraft maneuvers meant to accommodate time-related constraints in air traffic. Information related to flight performance and atmospheric conditions is gathered onboard an aircraft, then transmitted to an air traffic control center. In the event of a delay or any other event which necessitates an alteration in an aircraft trajectory, the data is sent to a decision support tool to compute and provide alternative trajectories, preferably including operator-preferred trajectories, within air traffic constraints. Air traffic controllers can then offer an alternative trajectory to an aircraft that is more efficient, cost effective, and/or preferable to the aircraft operator.

Abstract: A system and method for achieving vertical navigation by using a satellite based navigation system exemplified by a GPS system and implementing the vertical navigation features in an autopilot unit interfaced to the satellite based navigation system. The autopilot reads waypoint information output from the satellite navigation system and receives VNAV altitudes and other commands from the pilot. The autopilot then performs VNAV calculations and guidance in accordance with the VNAV program. VNAV setup and progressive status are displayed on an economical small screen autopilot display. Modes are disclosed for exemplary GPS direct to waypoint VNAV, waypoint transition VNAV, multiple waypoint VNAV and other VNAV modes. Safety limits may be imposed on the VNAV program.

Abstract: A system for managing vehicles on a road network includes a processor that performs operations including accessing a matrix of vehicle parameters of a plurality of communicating vehicles on the road network, and representing the plurality of communicating vehicles in a graph with a plurality of nodes corresponding to the plurality of communicating vehicles and with a plurality of edges corresponding to the vehicle parameters. The system can include partitioning, with the processor, the graph to reduce disruptions to the road network below a threshold level to support safe and efficient traffic flow, and assigning one or more exclusion zones within the road network to each partition of the graph by associating the vehicle parameters for each vehicle.

Abstract: An apparatus comprising a memory and a processor coupled to the memory, wherein the processor is configured to receive holding instructions for an aircraft, wherein the holding instructions comprise a holding fix, a holding direction, and an inbound leg course, obtain an airspeed for the aircraft, obtain a wind speed and a wind direction affecting the aircraft, calculate a holding pattern for the aircraft using the holding instructions, the wind speed, the wind direction, an inbound leg duration, and the airspeed, obtain Federal Aviation Administration (FAA) protected airspace limits associated with the holding fix, and present the holding pattern and the FAA protected airspace limits to a flight crew member on the aircraft.

Abstract: Methods and systems for determining a change of speed of an aircraft for enabling the avoidance of conflicts between aircraft trajectories. The method of determining a change in speed of an aircraft, comprises the steps of: defining a merge point and a tie point; monitoring a first aircraft; determining when the first aircraft passes the tie point; providing trajectory data; predicting a trajectory of a second aircraft using the trajectory data; defining a minimum permissible longitudinal spacing; predicting a longitudinal spacing between the first and second aircraft at the merge point based on the predicted trajectory; and if the minimum permissible longitudinal spacing is greater than the predicted longitudinal spacing then calculating a proposed change in speed of the second aircraft that will result in the longitudinal spacing between the first and second aircraft at the merge point being greater than or equal to the minimum permissible longitudinal spacing.

Abstract: A traffic control system sets a target value related to a travel state based on a correlation between a vehicle travel speed and a traffic volume, and controls multiple vehicles (CS) on a road in accordance with the target value as a common target value. The target value can be set based on a predicted traffic volume at a region (103) that is ahead of, in a vehicle travel direction, the multiple vehicles on the road. For example, the traffic control system sets, as the target value, a target speed or a target value of a parameter related to an inter-vehicle distance.

Abstract: A hybrid vehicle is provided in which after a determination is made as to whether the remaining capacity is higher than a first threshold value, any one of a first running mode, a second running mode, and a third running mode is selected depending on first speed, second speed, or third speed so that the vehicle runs in the mode, whereby the vehicle can run by easily selecting an appropriate series hybrid mode or an appropriate parallel hybrid mode in each range depending on whether the remaining capacity is higher than the first threshold value, and running control can be made stable and easy.

Abstract: A method and system for generating a dynamic speed limit is provided. The method includes dynamically receiving, from vehicles currently in motion on a roadway, a dynamically changing data stream comprising data comprising parameters associated with the vehicles. Speed limits, recommended lane assignments, and velocity ranges for the vehicles are dynamically defined. The speed limits, the recommended lane assignments, and the velocity ranges are transmitted to and presented by each associated vehicle.

Abstract: A system and method for managing vehicles on a road network can include a processor that performs operations including accessing a matrix of vehicle parameters of a plurality of communicating vehicles on the road network and representing the plurality of communicating vehicles in a graph with a plurality of nodes corresponding to the plurality of communicating vehicles and edges corresponding to the vehicle parameters. The system and method can include partitioning, with a processing device, the graph to reduce disruptions to the road network below a threshold level to support safe and efficient traffic flow and assigning one or more exclusion zones within the road network to each partition of the graph by associating the vehicle parameters for each vehicle.

Abstract: A control device (21) for a vehicle network, having a microprocessor (30) and a transceiver (40). The control device (21) can be switched off or switched to a sleep mode during a previously defined state or event during the operation of the motor vehicle and/or the control device (21) can be awakened from the sleep mode during a previously defined state or event during the operation. The disclosed embodiments also relate to a method for operating a vehicle network.

Abstract: A method is provided for guaranteeing a temporal spacing between an aircraft and at least one reference moving object, said spacing needing to be guaranteed no later than at a point in the flight plan called the point of interception, with the aircraft following a current flight plan. The feasibility of guaranteeing the spacing at a date Tcour by regulating the speed of the aircraft while maintaining the current flight plan is verified in a first step. In a second step it is verified whether the date Tcour is contained within a feasibility range. In a third step the current flight plan is modified when the feasibility is not verified, a lateral trajectory between the current position Xcour of the aircraft and the point of interception being implemented in this case such that the spacing can be attained by regulating the speed.

Abstract: Techniques are described for virtual traffic sensors (VTS). In an implementation, an electronic device provides a variety of functionality including at least functionality to determine position. The electronic device may be further configured to ascertain locations of one or more virtual traffic sensors. In at least some embodiments, locations of virtual traffic sensors are determined by the electronic device using a variety of VTS criteria. Using a determined position, the electronic device may detect proximity to the virtual traffic sensors. The electronic device may collect traffic related data when in proximity to the one or more virtual traffic sensors. The electronic device may then communicate the collected traffic data over a suitable network connection to a service provider.

Abstract: A visual/graphical air traffic display tool to aid flight crews in determining future heading/track and position of ownship based on current climb rate, bank angle and groundspeed under current meteorological conditions. The tool displays symbols which indicate the predicted future position and heading/track of ownship on a traffic display unit. The tool is also capable of using ownship's predicted position and information received from surrounding traffic to identify a future conflict at ownship's predicted position and then display a future conflict warning on the traffic display unit. In one embodiment, the future conflict warning takes the form of a change in the coloration of the ownship position and heading/track indicator being displayed.

Abstract: An apparatus comprising a memory and a processor coupled to the memory, wherein the processor is configured to receive holding instructions for an aircraft, wherein the holding instructions comprise a holding fix, a holding direction, and an inbound leg course, obtain an airspeed for the aircraft, obtain a wind speed and a wind direction affecting the aircraft, calculate a holding pattern for the aircraft using the holding instructions, the wind speed, the wind direction, an inbound leg duration, and the airspeed, obtain Federal Aviation Administration (FAA) protected airspace limits associated with the holding fix, and present the holding pattern and the FAA protected airspace limits to a flight crew member on the aircraft.

Abstract: A method and system for providing taxiway navigational information to a crewmember of an airplane taxiing at an airport. An airport taxiway navigation system (“ATNS”) that executes on an onboard computer system that displays a map of the taxiways of an airport, receives the name of each taxiway of the taxi route specified by the taxi clearance, and highlights the taxiways on a displayed map to provide a visual indication of the cleared taxi route for the crewmembers.

Abstract: A method and apparatus includes long term and short term strategies for improving 4D trajectory reliability and required time of arrival reliability. The long term strategy changes speeds along the trajectory to remove the time error in predictions. The short term strategy compensates for wind and position error, for example, by temporarily changing an aircraft guidance speed by applying a guidance margin that would either delay or prevent re-computation of the speed targets along the flight path. The predictions would use the original speed target without the guidance margin application. The guidance speed target will stay applied until the predicted time error crosses a threshold.

Abstract: A method for illustrating potential benefits resulting from revised navigation procedures to a customer is described. The method includes preparing a model for a revised navigation procedure, determining a landing probability for both an existing minimum separation procedure and a minimum separation determined utilizing the revised navigation procedure, calculating a benefit associated with a difference in the landing probabilities, and validating the revised navigation procedures through demonstration and use of the revised navigation procedure model on a computer-based flight simulation program.

Abstract: A method and device to help an aircraft change altitude in case of reduced separations is disclosed. The device, embarked on board the airplane, comprises means for determining a performing time range during which the altitude change maneuver within reduced spacings being desired by the pilots is able to be performed.

Abstract: A method and device establishes trajectory planning, predictions and guidance so as to obtain the satisfaction of a time constraint (RTA). This objective is achieved by undertaking a computation of a trajectory up to the point where the flypast time constraint applies, on the basis of a profile of altitude and speeds, and then by computing the profile of speeds and altitudes making it possible, throughout the computed trajectory, to comply with the RTA. The method is also a method for readapting the trajectory and the vertical profile when during a mission, the data outside the aeroplane have caused the time predictions to drift and the constraint is no longer complied with under the initial speeds and trajectory assumptions.

Abstract: A method for quickly calculating mileage includes the steps: A, receiving report data from a vehicular terminal and updating data center according to the report data; B, receiving an inquiry request which includes a vehicle number, a first time point which is earlier than a second time point and the second time point which are requested to inquire; C, inquiring the data center to acquire a first total mileage value to which the time point that is proximate to the first time point corresponds and a second total mileage value to which the time point that is proximate to the second time point corresponds; D, obtaining a running mileage L from the first time point to the second time point by subtracting the first total mileage value from the second total mileage value. A system for quickly calculating mileage quickly is also proposed.

Abstract: A device comprising a processor that detects an autonomously sensed change in a vehicle's operational state from an initial state characterized by a sensed vehicle speed equal to about 0; to an immediately succeeding vehicle state characterized by sensed vehicle speed being greater than about 0 and, verification from a reverse operating mode sensor that longitudinal vehicle speed is in a reverse direction; and presumptively signals the thusly detected change of vehicle operational state as an instance of reverse operation of the associated vehicle.

Abstract: Disclosed is a device and method of providing a driver with eco-driving information. More specifically, the disclosed method and device induces a driver to operate a vehicle in an eco-friendly manner by computing for and displaying to the driver a fuel efficiency oriented vehicle speed that maximizes the vehicle's driving distance based on the vehicle's current weight and electrical load.

Abstract: A method and apparatus for simulating effects of threats to aircraft communications. A simulation of an aircraft environment is run with the aircraft communications in an aircraft communications network in the aircraft environment. A number of conditions is introduced. The number of conditions comprises a threat configured to affect the aircraft communications in the aircraft communications network in an undesired manner. A change in traffic flow of aircraft in an airspace in the aircraft environment is identified in response to the number of conditions.

Abstract: A high-integrity auto-guidance and control method for use in conjunction with an aircraft electric taxi drive system comprises obtaining taxi path data generating in a plurality of processors taxi path guidance and control information from the taxi path guidance data, and sending commands derived from the taxi path guidance and control information from one of the plurality of processors based on a predetermined priority scheme to at least one electric taxi controller.

Abstract: A system is provided for controlling the speed of an aircraft during a deceleration segment between a first state associated with a first speed and a first time and a second state associated with a second speed and a second time. The system includes a navigation system configured to determine the first state; a guidance system configured to determine the second state; and an active deceleration system coupled to the navigation system and the guidance system and configured to construct the deceleration segment between the first state and the second state with at least one intermediate speed between the first speed and the second speed.

Abstract: Disclosed is a creep control system and method for a hybrid vehicle, which controls the driving of a motor according to the distance to a preceding vehicle in order to provide creep driving when the hybrid vehicle has come to a complete stop. In particular, driving information is detected and a determination is made as to whether the hybrid vehicle is in an idle stop and completely stationary state. Then when the hybrid vehicle is in the idle stop and completely stationary state, a determination is made as to whether a distance from a preceding vehicle is more than a predetermined distance. When the distance to the preceding vehicle is more than the predetermined distance, a motor is driven to perform creep driving.

Abstract: The present invention relates to methods of controlling the flight path of an aircraft to follow as closely as possible a predetermined four-dimensional flight path, such as when flying continuous descent approaches. A method of controlling an aircraft to follow a predetermined four-dimensional flight path is provided that comprises monitoring an actual along-track position and an actual vertical position of the aircraft relative to corresponding desired positions on the predetermined flight path. Throttle commands are generated based on deviations of the actual vertical position of the aircraft from the desired vertical position. Elevator commands are generated based on the deviation of the actual along-track position from the desired along-track position and on the deviation of the actual vertical position from the desired vertical position.

Abstract: A method and apparatus includes long term and short term strategies for improving 4D trajectory reliability and required time of arrival reliability. The long term strategy changes speeds along the trajectory to remove the time error in predictions. The short term strategy compensates for wind and position error, for example, by temporarily changing an aircraft guidance speed by applying a guidance margin that would either delay or prevent re-computation of the speed targets along the flight path. The predictions would use the original speed target without the guidance margin application. The guidance speed target will stay applied until the predicted time error crosses a threshold.

Abstract: A method or a system for displaying a traffic camera view of a road on a display within a vehicle. The method or the system may include monitoring a movement of the vehicle, determining an existence of a traffic event based on the movement of the vehicle, receiving a traffic camera view on the road, and displaying the traffic camera view if the traffic event is detected.

Abstract: A method includes receiving flight leg data and dispatcher position data for a planning horizon and identifying cycle flight legs and extraordinary flight legs based on the flight leg data. The method includes allocating each cycle flight leg to at least one dispatcher position while minimizing workload deviations between the dispatcher positions. The method includes allocating, after allocating each cycle flight leg, each extraordinary flight leg to at least one dispatcher position while minimizing workload deviations between the dispatcher positions.

Abstract: Avionics display system is provided for deployment onboard an aircraft and includes an air traffic data source that provides the avionics display system with data indicative of at least position and velocity of a neighboring aircraft. The system comprises a cockpit display system, and a monitor included within the cockpit display system. The cockpit display system receives and displays position and velocity data pertaining to the neighboring aircraft on the cockpit monitor as a position symbol and a velocity vector graphic. A processor operatively coupled to the monitor is configured to generate an air traffic display on the monitor including symbology indicative of (1) the current position of the neighboring aircraft (2) a velocity of the neighboring aircraft, and (3) the rate-of-change of the velocity of the neighboring aircraft.

Abstract: Methods and systems suitable for negotiating air traffic trajectory modification requests received from multiple aircraft that each has trajectory parameters. The methods include transmitting from at least a first aircraft a first trajectory modification request to alter the altitude, speed and/or lateral route thereof. A first conflict assessment is then performed to determine if the first trajectory modification request poses a conflict with the altitudes, speeds and lateral routes of other aircraft. If a conflict is not identified, the first trajectory modification request is granted and the first aircraft is notified of the first trajectory modification request being granted. Alternatively, if a conflict is identified, the first trajectory modification request is not granted and the first aircraft is notified thereof.

Abstract: A method for operating a longitudinal driver assist system of an automobile, in particular an ACC system, wherein environmental data of the automobile are evaluated with respect to travel in a longitudinal convoy with at least three automobiles which include the automobile and at least two additional automobiles, which are driving immediately behind one another and each have an active longitudinal driver assist system. A convoy value is formed, and at least one operating parameter of the driver assist system is adapted depending on the convoy value.

Abstract: A method for aiding the management of an aircraft flight according to an active flight plan receiving a control clearance transmitted at a current time includes a step of computing a reception flight plan based on the said control clearance, a step of storing the said reception flight plan in a memory space dedicated to the said reception flight plan. The method also includes, prior to the step of computing a reception flight plan: a step of determining the time, called the recognition time, assumed to have to elapse between the current time and a time at which the said control clearance is assumed to be recognized; a step of attribution, to the said control clearance, of a destination flight plan as a function of the recognition time, the said destination flight plan being the temporary flight plan when the recognition time is included in a first time slot and the destination flight plan being a secondary flight plan when the recognition time is included in a second time slot longer than the first time slot.

Abstract: A method and a device are described for scanning the surrounding environment of a vehicle. When the vehicle falls below a first boundary speed a timer is triggered whose state is incremented until the vehicle exceeds a boundary speed, a check of the unobstructed view of the scanning device being carried out upon expiration of the time period recorded by the state of the timer and in which the state of the counter is incremented.

Abstract: A method of transferring and processing flight data of an aircraft including recording the aircraft flight data in an onboard avionics system in a digital format so as to obtain digital data, the flight data including safety impact flight data and flight data having no recognized effect on safety. The method further includes recording at least the safety impact flight data in the onboard avionics system in an additional format dissimilar to the digital format so as to obtain additional flight data, storing the digital data and the additional flight data separately, transferring the digital data and the additional flight data to a monitoring computer on the ground, displaying the digital data on a screen in the form of display digital data, and transferring the digital data and the additional flight data to a complementary interpretation unit so as to generate one of display data and print data relating to the additional flight data.

Abstract: Methods and apparatuses for estimating a user's altitude with respect to the mean sea level are provided. According to some aspects, the present invention is able to estimate altitude in both open sky as well as in degraded GPS signal environments such as dense urban canyon environments where GPS performance is affected by fewer available satellites and/or multipath error. According to other aspects, the present invention uses data from a pressure sensor to estimate altitude, either with or without the use of GPS aiding data. According to further aspects, estimated altitude is integrated with other types of dead reckoning data to provide user context detection pertaining to changes of altitude.

Abstract: A method for achieving and maintaining spacing between aircraft may include receiving by a following aircraft information related to a lead aircraft. The information is useable for achieving and maintaining spacing by the following aircraft from the lead aircraft. The method may also include determining spacing of the following aircraft from the lead aircraft. The method may additionally include receiving by the following aircraft a vertical profile for the traffic management environment. The method may further include automatically controlling throttle settings to achieve and maintain spacing by the following aircraft from the lead aircraft while maintaining the vertical profile of the following aircraft in response to an automatic spacing mode being enabled.

Abstract: Described herein are systems and methods for surface management of an airport. One embodiment of the disclosure of this application is related to a method including receiving airport data from an airport network, receiving surface surveillance data for specific segments of an airport area, identifying predicted conflicts within one of the segments based on the airport data and surface surveillance data, and allocating a taxi time slot for the flight. Another embodiment of the disclosure of this application is related to a system comprising a user interface displaying information related to flight plan data and airport data received from an airport network, and a surface management module receiving the airport data and surface surveillance data for specific segments of an airport area, identifying predicted conflicts within one of the segments based on the airport data and surface surveillance data, and allocating a taxi time slot for the flight.

Abstract: The invention relates to a method and device for automatically managing the separation between two aircraft following one another. The device (1) comprises a means (6, 7) for automatically calculating, prior to performing a function to acquire and maintain separation, orders for controlling speed that enable a trailing aircraft to acquire and maintain a time separation relative to a target aircraft preceding the former.

Abstract: A system and method for aircraft taxi gate selection based on passenger connecting flight information. In one embodiment, a communication link is established between an aircraft computing system and a ground station system via a communication network provided by the ground station system. Further, aircraft taxi gate selection information and the passenger connecting flight information are substantially simultaneously displayed on a display device to a pilot upon establishing the communication link. Furthermore, the pilot is allowed to select an aircraft taxi gate based on the displayed aircraft taxi gate selection information and passenger connecting flight information.