Abstract: The invention provides, in some aspects, flight management systems and methods that generate three-dimensional (3D) graphical representations of airspace in a vicinity of an aircraft (e.g., in flight or during take-off). Such systems can include a display and a processor that drives the display to generate a two-dimensional (2D) or three-dimensional (3D) depiction of flight path. In a first mode, the processor drives the display to generate a flexible highway-in-the-sky (HITS) fight path having an endpoint that is fixed to a destination and having an origin that moves relative to a current location of the aerial vehicle (e.g., a path that “stays” with the vehicle). In a second mode, the processor drives the display to generate a depiction of a fixed HITS flight path that is fixed as to origin and destination and that does not move relative to the craft.

Abstract: Techniques are described for providing a meeting notification and automatic modification service. A system may be configured to identify an appointment in a calendar application, identify a geographic location of the appointment, and identify, before the appointment time, a geographic location of a first participant of the appointment. Based on the geographic information, the system may identify a route extending from the geographic location of the first participant to the geographic location of the appointment, and may identify a travel time associated with the route. Based on the travel time and the appointment time, the system may determine whether the first participant is estimated to arrive at the appointment on time and, based on the determination, the system may send a message to participants of the appointment or dynamically reschedule the appointment.

Abstract: A method of operating a hybrid transmission includes controlling the transmission according to a drive mode, which includes a continuously variable speed relationship, and controlling the transmission according to a fixed speed relationship mode, which includes a plurality of fixed speed relationships including mechanical gear ratios and virtual gear ratios.

Abstract: In a method for operating an internal combustion engine of a motor vehicle, a driver type is ascertained. A criterion for performing a diagnosis or a regeneration of a component of the fuel supply system is a function of the ascertained driver type.

Abstract: A system and method for determining and displaying an overall efficiency value of a vehicle. The vehicle may include an engine and an electric machine that operates to provide torque to propel the vehicle. In addition, the vehicle may have an electric power source that provides electric power to the electric machine. A controller may determine and transmit the overall efficiency value so that the information display displays the number of efficiency indicators. Also, the number of efficiency indicators displayed may be based on the overall efficiency value.

Abstract: An electronic mobile device includes a display, a tilt sensor and a processor. The display is for displaying a graphical element. The tilt sensor is configured to measure a tilt angle of the mobile device. The processor is configured to store the measured tilt angle as a reference tilt angle, subsequently determine a delta tilt angle as the difference between a currently measured tilt angle and the reference tilt angle, compare the delta tilt angle to different thresholds, and alter the position of the displayed element on the display at a rate that is based on the number of the thresholds the delta tilt angle has exceeded.

Abstract: This system for displaying, on the flight deck of an aircraft travelling on the surface of an airport, an airport map mentioning the surface traffic, for the purpose of a taxiing aid and protection of the ground movements of the aircraft, shows on the airport map only the traffic occupying the airport thoroughfares close to the aircraft, this closeness being defined by the existence of a joining path comprising a number of thoroughfare sections that is less than an arbitrary limit of the order of 1 or 2.

Abstract: A navigation device with power saving mechanism and method thereof are provided. The navigation device includes a global positioning system (GPS) receiver, a first processing unit, a second processing unit and a sound playing unit. The GPS receiver produces a longitude-latitude information by receiving a satellite signal from the GPS. The first processing unit switches from a first mode to a second mode according to a control signal. Then, the first processing unit is disabled after switching. When the second processing unit is enabled, a direction information and a distance information are generated by comparing the longitude-latitude information with a destination information. The sound playing unit selects two frequencies among a plurality of navigation frequencies according to the direction information and the distance information, and plays the tone signals which are comprised of the two frequencies in sequence.

Abstract: The intelligent system for autonomous spacecraft operations includes an on-board Autonomous Operations subsystem integrated with an on-ground Web-based Remote Intelligent Monitor System (RIMS) providing interface between on-ground users and the autonomous operations intelligent system. The on-board Autonomous Operation subsystem includes an On-Orbit Checkout Engine (OOCE) unit and an Autonomous Tasking Engine (ATE) unit. Spacecraft Command Language (SCL) engine underlies the operations of the OOCE, ATE and RIMS, and serves as an executer of commands sequences. The OOCE uses the SCL engine to execute a series of SCL command scripts to perform a rapid on-orbit checkout of subsystems/components of the spacecraft in 1-3 days. The ATE is a planning and scheduling tool which receives requests for “activities” and uses the SCL scripts to verify the validity of the “activity” prior to execution, and scheduling the “activity” for execution or re-scheduling the same depending on verification results.

Abstract: The communication system including a master device and a plurality of slave devices communicatably connected to the master device is configured such that a selected one of the slave devices which is applied with a communication permission signal from the master device through a corresponding one of control lines performs communication with the master device. The master device includes a switching circuit that changes internal connection thereof such that the communication permission signal is applied to another one of the slave devices which should perform communication with the master device next.

Abstract: The present invention relates to a method and a system for monitoring the following of a reference trajectory by an aircraft.

Abstract: A remote data concentrator receives signals from a plurality of sensors. The plurality of sensors are for use on an aircraft. Each of the sensors have their signals split between at least two flow paths, such that each of the sensors are provided with redundancy. The remote data concentrator is also utilized as part of an aircraft electrical control system.

Abstract: An apparatus, and related method, for monitoring and controlling the traffic of transport systems, such as railway vehicles, wherein the vehicles include device elements, such as satellite positioning systems, monitored by a series of centralized units to monitor and control adjacent areas. In case of anomalous traffic situations, the system and method provides proper alarm signals and signals for automatically putting into action the breaking systems of the vehicles. To do so, the devices can interface with breaking means and sensors placed along the railway paths and in the vehicles, and exchange positioning data or other kinds of data of various sensors, among vehicles running within a certain mutual distance and can further include a secured memory means for storing data, information and parameters.

Abstract: A system and method are disclosed for managing a network of sensors (100). A system that incorporates teachings of the present disclosure may include, for example, a sensor (102) belonging to the network of sensors operating in a geographic space having a controller (210) that manages a sensing device (204). The controller can be programmed to locate (302) itself in the geographic space, and assign (304) itself according to its location a zone within a portion of the geographic space and a corresponding data range for storing sensed information. Additional embodiments are disclosed.

Abstract: Arrangement and method for managing information about the condition of travel lanes on which vehicles travel includes a sensor system arranged in each vehicle for obtaining information about the maintenance state of the travel lane, a communication system arranged in each vehicle and coupled to a respective sensor system for communicating the obtained information to a control station, and a transmission system arranged at or coupled to the control station for transmitting the obtained information to vehicles other than the one which provided the obtained information. A positioning system may be arranged on each vehicle to determine its position and the communication systems transmit the position of each vehicle along with the obtained information.

Abstract: An aircraft flight control surface actuation control system includes an actuator control unit and a flight control module. The actuator control unit includes at least two independent actuator control channels to generate limited authority flight control surface actuator commands based on pilot inceptor position signals and flight control augmentation data. The flight control module supplies the flight control augmentation data to each of the independent actuator control channels, determines operability of each of the actuator control channels and, based on the determined operability of each independent actuator control channel, selectively prevents one of the independent actuator control channels from supplying the limited authority flight control surface actuator commands. The flight control module may also generate full authority flight control surface actuator commands for supply to flight control surface actuators.

Abstract: The subject of the present invention is a method for improving route and 4D prediction calculations by FMS in the framework of ATC tactical flight instructions, which method enables the FMS of an aircraft to carry out its usual predictions as precisely as possible when it has left or anticipates leaving its initial flight plan following an instruction from the air traffic controller, and has no instructions telling it where and when to return to the initial flight plan, and the invention is characterized in that it consists in transmitting to the aircraft, from an air traffic control centre, information enabling the FMS system to be aware of traffic crossing points (X1) and control sector changes, and to use this information to predict the coordinates of a point (X2) at which it is supposed to rejoin its initial flight plan at the earliest opportunity after the crossing point that required an alteration of trajectory and at the latest opportunity on the last point of the current sector.

Abstract: A method for policing and managing the operation of a flying, unmanned aircraft in the event of usurpation of control of, malfunction of, or ill-intentioned use of, this aircraft includes the steps of (a) detecting inappropriate operation of the aircraft; (b) transmitting a takeover command to the aircraft to interrupt control of the operation of this aircraft by a first pilot and relinquish control of the aircraft to a second pilot; and (c) transmitting control commands to the aircraft to control its operation by the second pilot, until the need for alternate pilot control of the aircraft has ended or until the aircraft has landed safely.

Abstract: A navigation apparatus acquires weather information along a navigation route to a destination from an information center and calculates an importance that is assigned to the weather information based on a predetermined criterion as well as a determination mode and a travel purpose inputted from a user. The importance of the weather information may be calculated by employing an importance calculation table that defines importance of the weather information itself or the importance of the weather information relative to the navigation route. The importance of the weather information is used to extract a required part of the weather information for providing the user with the information. The weather information extraction may be performed according to a criterion such as extracting the weather information with a certain importance level or higher, extracting the weather information of top n th importance, or the like.

Abstract: A control unit for personal protection having a polarity reversal protection between an external battery voltage and an internal voltage, to prevent an energy discharge from the control unit. The control unit also has a bidirectional DC/DC converter between an energy reserve and the internal voltage, the DC/DC converter determining its direction of conversion as a function of the internal voltage. The control unit is configured so that the control unit, after a switching-off process, records at least one measured value and generates a signal as a function of this measured value which characterizes an autarchy behavior of the control unit.