A communication control device for a subscriber station of a serial bus system. The communication control device has a communication control module for generating a transmitted signal for controlling a communication of the subscriber station with at least one other subscriber station of the bus system, in which bus system at least a first communication phase and a second communication phase are used for exchanging messages between subscriber stations of the bus system, a first terminal for transmitting, in an operating mode of the first communication phase, the transmitted signal to a transmitting/receiving device, a second terminal for receiving, in the operating mode of the first communication phase, a digital received signal from the transmitting/receiving device, and an operating mode switching module for switching the transmission direction of the first and the second terminal in the second communication phase to the same direction for differential signal transmission.

A distributed air data module system includes several air data systems and a control module communicatively connected to each air data system via a data channel. Each of the air data systems includes a sensor that is configured to sense an air data parameter and to provide a sensor output signal that is indicative of the sensed air data parameter, and a sensor analog-to-digital converter that produces a digital air data parameter signal that is representative of the sensor output signal. Each air data system has an associated air data system address code. The control module is configured to generate a selected air data system address code corresponding to a selected air data systems, receive the digital air data parameter signal associated with the selected air data system via the data channel, and transmit the digital air data parameter signal via an aircraft data bus.

A system for virtualizing a plurality of controller area network bus units communicatively connected to an aircraft, the system comprising a plurality of physical controller area network bus units, each is configured to detect a measured state datum of a plurality of measured state data of the aircraft; and transmit the plurality of measured state data to at least a network switch, the at least a network switch configured to receive the plurality of measured state data from the plurality of physical controller area network bus units, generate a single transmission signal as a function of the plurality of measured state data, and transmit the single transmission signal to a computing device, and the computing device configured to receive the transmission signal originating from the at least a network switch, and bridge each virtual controller area network bus unit of the plurality of virtual controller area network bus units.

The avionic system of an aircraft includes a set of avionic computers and a switch associated with each avionic computer. For each avionic computer of the set of avionic computers, the avionic system includes a communication link between the switch associated with this avionic computer and each of the switches associated with the other avionic computers. Each switch is configured such that it routes the data frames received on its input ports to its output ports in a manner predefined only on the basis of the input ports on which these data frames are received. The various switches are configured such that, when an avionic computer sends a data frame, this data frame is transmitted to all of the other avionic computers.

Methods of guaranteed reception and of processing of a digital signal in an avionics system comprise a plurality of computers, each computer comprising processing electronics and a software layer, which, on receipt of an event, carries out the following steps: at a first instant, sending to each of the other computers of a first signal (ACK) of reception of the event; at a second instant termed “TimeOut ACK”, if the electronic computer has not received one of the first signals emanating from one of the other computers, sending of a second failure signal (FAIL) to each of the other computers; at a third instant termed “TimeOut GARANTEED”, if a second failure signal has been received by the computer, absence of taking into account of the event by the computer and if no failure signal has been received by the computer, taking into account of the event by the data processing electronics of the computer.

The subject matter disclosed herein relates to a frame switch of an AFDX network in which the data acquisition application is decentralized. When the switch has to acquire the data transmitted on a virtual link, the switching table contains, apart from the input port and the output port (s) taken by this link, an ID representing the MAC address of the switch. The frames of this link are then not only switched but also transmitted to the network interface of the switch and processed by a dedicated application (DDA), hosted inside the switch. This application can be interrogated by a remote server and transfer the data that it has stored locally.

Systems and methods for regulating communications in computing systems are provided. For instance, a computing system can include a first processing board including a first processing device and a first control device. The system can further include a second processing board including a second processing device and a second control device. The system can further include a communications interface communicatively coupled to the first processing board. The communications interface includes one or more input/output ports configured to facilitate communication between the avionics system and one or more external devices. The first control device of the first processing board is communicatively coupled to the second control device of the second processing board via a shared bus. The first control device is configured to regulate communications associated with the communications interface.

A centralized control system and/or method for controlling an aircraft are provided. The centralized control system includes a controller configured to receive a device signal and transmit a control signal, a communication bus connected to the controller being configured to transport the device signal and the control signal, a plurality of devices connected to the controller using the communication bus, wherein at least one of the plurality of devices includes at least one of a sensor being configured to collect the device signal and an effector configured to respond to the control signal, and a bus communication circuit configured to communicate over the communication bus to the controller.

An aircraft data network is provided that can include a first Remote Data Concentrator (RDC), a network switch and a second RDC. The first RDC can receive one or more input signals comprising data from a transmitting system, and translate the data per a network protocol to generate translated data having a format in accordance with the network protocol. The network switch can receive the translated data from the first RDC, determine a destination for at least some of the translated data, and route at least some of the translated data toward a first receiving system. The second RDC can receive at least some of the translated data from the network switch, convert at least some of the translated data to generate converted data having a format designed for use by the first receiving system, and communicate the converted data to the first receiving system.

Hybrid wire-fiber data networks that include wire-fiber transceivers protected against environmental interferences. In some embodiments, a hybrid-wire-fiber data network of this disclosure provides a fiber-optic link between portions of one or more wired networks. In some embodiments, a hybrid wire-fiber data network of this disclosure includes a fiber-optic link that relies only on message-priority arbitration performed on wired portions of one or more wired networks. In some embodiments, a wire-fiber transceiver of this disclosure includes electromagnetic environment (EME) protective circuitry for one or both of input power and input signals. In some embodiments, a wire-fiber transceiver of this disclosure is configured for use with a controlled area network media-access protocol (CAN) and/or a derivative of CAN. Various data communication and other methods are also disclosed in addition to hybrid wire-fiber data networks and components thereof.