537 results about "Flight management system" patented technology

The present invention is a system and method for providing flight management to one or more aircraft via a communication link between a fight management system located outside the aircraft and a flight management system located inside the aircraft. Remote flight management system may monitor and control navigation functions, substantially reducing pilot or crewmember workload. Optimized simultaneous flight management of multiple aircraft located within a specified area or within a specified fleet may be provided. Remote flight management system may be suitable for monitoring and controlling navigation functions for multiple aircraft from a single location.

Methods and apparatus for managing multiple user access control entities or clients. For example, in one embodiment, a “wallet” of electronic subscriber identity modules (eSIMs) may be stored and used at a user device and / or distributed to other devices for use thereon. In another embodiment, a networked server may store and distribute eSIM to a plurality of user devices in communication therewith. A database of available eSIM is maintained at the wallet entity and / or at the network which enables request for a particular eSIM to be processed and various rules for the distribution thereof to be implemented. Security precautions are implemented to protect both user and network carrier specific data as the data is transmitted between networked entities. Solutions for eSIM backup and restoration are also described.

Methods, systems, and apparatuses for the use of a wireless portable avionics device in conjunction with on-board flight systems and / or off-board service providers. The device may be used by aircraft personnel such as pilots and may act as a command / data entry and / or display tool to augment cockpit display systems. The device can receive flight data (e.g., a flight plan) from an off-board provider and automatically transfer it, as well as any previously prepared commands or data, to a flight management system and / or cockpit display systems. Commands and / or data (including pre-existing ones and ones entered in real-time) can be wirelessly transferred to the on-board flight systems which are not in direct physical contact with the device. Thus, the device can be easily manipulated during turbulence or under poor readability conditions. The device can be used to manipulate items shown on cockpit display systems in a timely and accurate manner.

A system and method is disclosed for measuring time of flight to an object. A transmitter transmits an electromagnetic signal and provides a reference signal corresponding to the electromagnetic signal. A receiver receives the electromagnetic signal and provides a response signal corresponding to the received electromagnetic signal. A detection circuit is configured to determine a time of flight between the transmitter and the receiver based upon the reference signal and the response signal.

A system and method is provided for transmitting, receiving, initiating, and displaying textual air traffic control clearance messages simultaneously with a graphic representation of an aircraft flight plan. Data representative of a current aircraft flight plan, and one or more textual clearance message signals representative of air traffic control clearance message, are each processed. One or more images representative of the current aircraft flight plan, and one or more images representative of the textual air traffic clearance messages, are each substantially simultaneously displayed in the same display area of a flight management system display.

The present invention provides systems, apparatus and methods for entering data into a flight plan entry field which facilitates the display and editing of aircraft flight-plan data. In one embodiment, the present invention provides a method for entering multiple waypoint and procedure identifiers at once within a single a flight plan entry field. In another embodiment, the present invention provides for the partial entry of any waypoint or procedure identifiers, and thereafter relating the identifiers with an aircraft's flight management system to anticipate the complete text entry for display. In yet another embodiment, the present invention discloses a method to automatically provide the aircraft operator with selectable prioritized arrival and approach routing identifiers by a single manual selection. In another embodiment, the present invention is a method for providing the aircraft operator with selectable alternate patterns to a new runway.

In one embodiment, a pressure sensing system is described which transmits data to a patient management system external to a patient. The pressure sensing system can rigidly couple to an implantable port or flexibly couple to an implantable port. In some embodiments, the pressure sensing system communicates with a hydraulic actuating system. In some embodiments, the pressure sensing system is implantable and comprises a circuit capable of wireless transmission through the skin of a patient to an external receiver which is part of a patient management system. A patient management system is described which receives up to date as well as historical data from the pressure sensing system and manages the these data in the context of a patient database.

A system for tracking a ground imaging apparatus includes a plurality of fixed devices and at least one tracked device. The fixed devices are positioned at fixed locations and the tracked device is affixable to the ground imaging apparatus. The fixed devices and the tracked device are configured to transmit and / or receive signals used for time of flight measurements. A processor is configured to determine one or more positions of the tracked device relative to one or more of the fixed devices based upon one or more time of flight measurements between the tracked device and one or more of the fixed devices.

A method of optimizing a flight plan of an aircraft used in a flight management system of an aircraft is disclosed. This method makes it possible to constrain the real cost index of the mission executed to the optimal cost index CIopt predetermined by the aircraft operator, by acting on objectives ETAopt and EFOBopt of values of ETA and of EFOB to be achieved. Objectives are linked to this optimal cost index, in order to make the system return from a cost index CIm to the optimal cost index CIopt, while taking account of various constraints imposed by the ATC or the CTFM. Both constraints mext influence the cost index and constraints which limit the field of possible solutions.

System and method increase the visibility of critical flight information on electronic displays. An aircraft display system includes a processing unit, a flight management system, a navigation system, a database for storing target data and terrain data, a graphics display generator, and a visual display. The flight management system and / or the navigation system provide real-time aircraft operational and flight control information. The processing unit directs the graphics display generator to generate graphic control signals for the visual display, which increase the transparency of a segment of a zero pitch reference line in the vicinity of a flight path marker on the display.

An unmanned aerial vehicle (UAV) delivery system, for delivering articles between UAV zones has a computing system having a non-transient memory with executable instructions, the executable instructions including a flight management system to receive at a portal a delivery request to deliver an article from one zone to another. The Instructions are operable: to assign a UAV to the delivery request; if a UAV is not at a first zone, to dispatch a UAV to the first zone; to provide a flight path to the UAV,I at least part of the flight path being predetermined; to communicate the UAV flight path to the UAV; and to monitor the flight of the UAV from the first zone to the second zone and the delivery of the article. A method of planning a route for an unmanned aerial vehicle (UAV) is also provided.

The invention provides a general aviation flight monitoring airborne system based on an ADS-B (Automatic Dependent Surveillance-Broadcast). The system comprises an airborne ADS-B transceiver based on UAT (Ultra Aperture Terminal)\1090ES (Echo Sounding), a message processor based on the ADS-B and an airborne CDTI (Cockpit Display of Traffic Information) based on the ADS-B. The system provided by the invention has an ADS-B OUT / IN function and can be used for coding information input by an airborne FMS (flight management system), a GNSS (Global Navigation Satellite System), a barometric altimeter and a pilot, generating a message and broadcasting the message; and the system can receive flight status ADS-B messages of other airplanes and ground monitoring messages and separate UAT signals from 1090ES signals by virtue of a UAT data chain and a 1090ES data chain. The system provided by the invention can be used for respectively verifying, storing and parsing the flight status of the other airplanes\ground monitoring messages, messages of a local airplane, heartbeat messages of a host, graphical display navigation information, traffic information of the local airplane and traffic information of the other airplanes within a certain range of the local airplane.

The present invention lies in the field of embedded flight management systems on board aircraft. The invention relates notably to a system for managing alerts and procedures, and more precisely to a device for managing piloting tasks carried out by a crew of an aircraft. The device for managing tasks (1) according to the invention comprises:a module for managing alerts (4) generating alerts as a function of information originating from systems (2) of the aircraft, said module for managing alerts (4) being associated with a first display system (5) and with a first monitoring panel (7);a module for managing tasks (8) creating a task on receipt of an alert requiring at least one action on the part of the crew, creating a task associated with a procedure, said module for managing tasks (8) being associated with a second display system (11) and with a second monitoring panel (14);a module for managing a procedure (16) corresponding to a task selected by the crew, said module for managing a procedure (16) being associated with a third display system (17) and with a third monitoring panel (18).

The invention belongs to the technical field of construction site digital management and particularly relates to a construction site digital management system and an application method thereof. The management system comprises five sub systems, namely, a PLS (personnel location system), an access control system, a material management system, a shield operating system and a duct piece tracking system, wherein all the sub systems are connected with a remote database server, five sub database corresponding to the five sub systems are established in the remote database server, all the sub systems perform read-write operation on a main management object in a construction site range by using an RFID (radio frequency identification) technology, read data are uploaded to all corresponding sub databases in real time, and the operating authorization of a handheld RFID read head and the operating authorization of a shield machine are obtained through cross verification of data among all main sub databases. The management system and the application method have the advantages as follows: conventional extensive management is improved, the management responsibility is cleared, the management level is improved, and engineering information management, digital management and visual management are realized.

The invention relates to a device for assisting in the choice of a diversion airport for an aircraft piloted by a crew (200), said aircraft comprising a flight management system including location means (207) calculating the position of the aircraft, said device comprising a navigation database (202) and a performance database (203) of the aircraft, said device being characterized in that it comprises:a company database (201) comprising airports and characteristics of said airports,means (205) of calculating a list of airports, called candidate airports, from the airports in the company database, from the navigation database and from the selected characteristics by the crew,means (204) for calculating remaining flight time and fuel consumption predictions for each of the candidate airports from the position of the aircraft, from weather conditions and from the performance database,an interface giving the favoured airports for diversion according to pre-established criteria or determined in real time using the interface.

A method of creating and modifying a flight plan using a cursor control device and a display to represent the flight plan in the context of terrain. The method includes inserting waypoints, including origin and destination waypoints, into a flight plan using a cursor control device to position the waypoints in a display and commanding a flight management system (FMS) to connect the waypoints into a flight plan. The flight plan is drawn in the context of terrain on a display where conflicts between the flight plan and terrain are indicated. Selected elements of the flight plan are selected with a cursor control device and the selected elements are dragged to new positions on the display until terrain conflicts are eliminated, thus generating a modified flight plan. The modified flight plan is reviewed in the context of terrain to determine its acceptability and making further modifications thereof if desired. The modified flight plan is selected from the review thereof, the modified flight having no conflicts with terrain. Finally, the modified flight plan is activated using the FMS.

A flight management system for an aircraft, for executing a flight plan comprising referenced waypoints comprising a start point, an end point and intermediate waypoints, the said aircraft having a specified fuel quantity at the start of the said flight plan, executes a function of monitoring the fuel consumption with respect to at least one threshold value. The function comprises an operation for estimating if the quantity of fuel remaining on board drops below a threshold at any point in the flight plan included between the start point and the end point, and inserts a corresponding pseudo-waypoint in the flight plan, corresponding to the point where the said threshold is passed. The inserted pseudo-point is displayed on screens for displaying the flight plan.

Methods and apparatus are provided for interactively building flight paths for entry into an aircraft flight management system (FMS). The apparatus comprises a database containing map information, a display for presenting the map information, a user controlled cursor and selection buttons, all under the control of a graphics processor. The processor presents the map information with included navigation features on the display, correlated with the aircraft position and cursor location. When the cursor overlies a navigational feature (airways, waypoints, etc.), the processor highlights the feature. Feature ID information may also pop up when the feature is highlighted. Using a mouse button or equivalent, the user selects the highlighted feature or ID, whereupon the processor sends the information associated therewith to the FMS. By successively highlighting and selecting features or IDs an entire flight path can be identified and entered automatically into the FMS without the need for individual text entry.

The invention discloses an intelligent tool cabinet and relates to intelligent warehouse management systems. The intelligent tool cabinet is composed of a control system, a computer management system, a cabinet body, a touch computer, RFID antennas, audible and visual alarm devices, proximity switches, travel switches, a one-dimension code and two-dimension code scanner, an RFID reader-writer, a control board card, electric control locks, a user account collecting device and the like. A modern automatic control technology and a computer information management technology are integrated, and the intelligent tool cabinet has various management application functions of borrowing and returning record inquiry, report generating, management of authorities of staff, returning reminding, regular checking reminding, configuration analysis and others and can be used for storing various tools or articles, so that unmanned management of tool borrowing and returning is achieved. Information sharing can be achieved between the intelligent tool cabinet and various management systems, reliability is high, the requirement for strictly managing the tools of occasions is met, and the intelligent tool cabinet is widely applied to the fields of aerospace, electric instrument and military instrument management and others.

A method and apparatus for docking a spacecraft. The apparatus comprises elongate members, movement systems, and force management systems. The elongate members are associated with a docking structure for a spacecraft. The movement systems are configured to move the elongate members axially such that the docking structure for the spacecraft moves. Each of the elongate members is configured to move independently. The force management systems connect the movement systems to the elongate members and are configured to limit a force applied by the each of the elongate members to a desired threshold during movement of the elongate members.

A flight management system for an aircraft may determine maneuvers to avoid loss of separation between the aircraft and another aircraft. The flight management system may include a processor and a memory accessible to the processor. The memory may store instructions that are executable by the processor to identify a potential loss of separation between the aircraft and a second aircraft. The instructions may also be executable by the processor to determine whether executing a first speed maneuver using predetermined parameters is predicted to avoid the potential LOS. The instructions may be further executable by the processor to determine parameters of a second speed maneuver when the first speed maneuver is expected to avoid the potential LOS.

A user interface for an integrated autopilot and flight management system for an aircraft includes a plurality of tactical parameter controls for operation of the autopilot and a plurality of strategic parameter controls for operation of the flight management system.

The invention provides a priority management system of a nuclear power plant; the priority management system of the nuclear power plant is mainly used for managing instruction priorities and interfaces among a digital instrument control system and other systems of the nuclear power plant and driving devices of engineered safety facilities; the priority management system is used for directly receiving instructions from an engineered safety driving cabinet ESFAC, a safety related control cabinet SRC, a diversified driving control cabinet DAC, a serious accident control cabinet SAC and a power plant standard automatic system PSAS in a hard wiring manner, collecting feedback information of a field executor, supporting a self-diagnostic function and a periodic test of a safety system, and transmitting the feedback information, a self-diagnostic result, a quantitative test result and the like of the field executor to a DCS (Data Communication System) of the nuclear power plant; the priority logic part of the priority management system is in the form of a logic circuit; therefore, the priority management system is completely different from the DCS; and thus, software common-cause failures can be effectively avoided.

A computer-implemented method for managing the data of an aircraft flight plan comprises collecting initial data of an operational flight plan from a flight planning system FPS by an electronic device of electronic flight bag EFB type; converting the initial data and communicating the converted data to the avionics system of the flight management system FMS, the FMS being able to compute an avionic flight plan on the basis of the converted data; and retrieving the avionic flight plan data such as processed by the flight management system FMS. Developments describe notably the verification of the security and / or of the integrity of the converted initial data by means of predefined compliance rules; the emulation of avionics protocols and the use of the encipherment of the data. System aspects and software aspects are described.

An aircraft flight management system having a flight management computer that stores a pre-planned lateral route of flight of the aircraft comprising a plurality of successive waypoints to be overflown, the next proximate waypoint being an active waypoint, a method providing a return-to-path maneuver in the event that the aircraft deviates from the pre-planned route, including selecting a new active waypoint, calculating a return-to-path route to overfly the new active waypoint, and selectably accepting the calculated return-to-path route.

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.

The invention relates to a flight management system for manned or unmanned aircraft having to face an emergency situation such as hijacking of the aircraft, medical emergencies, situations of failures affecting the propulsion, pressurization or communication functions for example. It provides for a device and process for automatically or semi-automatically generating a flight plan compatible with international regulations and their national or local adaptations with possibilities of optimization according to navigation parameters.

An aircraft taxiing system is provided, comprising a flight control system, an electric taxi system having controls, a flight management system (FMS), at least one data input source coupled to the FMS, and a traffic collision avoidance system (TCAS). The FMS is programmed with instructions to calculate guidance speed and heading commands, augment the guidance commands to avoid runway incursions, and transmit the guidance commands to the flight control system. The TCAS is programmed with instructions to receive Automatic Dependent Surveillance-Broadcast (ADS-B) data from ground traffic, generate collision avoidance alerts; and transmit the collision avoidance alerts to the flight control system. The flight control system is programmed with instructions to receive guidance commands from the FMS, receive the traffic collision avoidance alerts from the TCAS, and compute the steering commands, and transmit the commands to the electric taxi system to taxi the aircraft along a calculated taxi route.