Abstract: An aircraft control system including transducers connected by interface units to an avionics network, such as an AFDX network. Each transducer is directly connected to an interface unit local to the transducer. Each interface unit is a configurable unit and has a signal processing module converting data to a format suitable for transmission over the network. Each interface unit may be configurable, via software commands, to operate in an application session mode, a data-loading mode, or a maintenance mode. Each interface unit may be directly associated with one of the software applications of the aircraft control system. The network may include a lower bandwidth part where data communication is conducted over sampling ports only. Interface units may be configured or installed using a plug and play method.

Abstract: A system for broadcasting an avionics temporal reference over a set of devices (7) of an aircraft, the system includes a master clock (5) configured to broadcast the avionics temporal reference via a wireless communication network (3) according to at least one predetermined frequency belonging to a wireless avionics intra-communication frequency band.

Abstract: A system for broadcasting an avionics temporal reference over a set of devices (7) of an aircraft, the system includes a master clock (5) configured to broadcast the avionics temporal reference via a wireless communication network (3) according to at least one predetermined frequency belonging to a wireless avionics intra-communication frequency band.

Abstract: An aircraft control system including transducers connected by interface units to an avionics network, such as an AFDX network. Each transducer is directly connected to an interface unit local to the transducer. Each interface unit is a configurable unit and has a signal processing module converting data to a format suitable for transmission over the network. Each interface unit may be configurable, via software commands, to operate in an application session mode, a data-loading mode, or a maintenance mode. Each interface unit may be directly associated with one of the software applications of the aircraft control system. The network may include a lower bandwidth part where data communication is conducted over sampling ports only. Interface units may be configured or installed using a plug and play method.

Abstract: The disclosure relates to a system embedded in an airplane comprising an electronic device intended to be inserted into a frame, a frame that can accommodate the electronic device, in which system the electronic device includes a radiofrequency tag reader, a radiofrequency tag, having a configuration information item, is fixed to the frame such that the radiofrequency tag reader can read the radiofrequency tag once the electronic device is inserted into the frame and the electronic device is adapted to, in a phase of configuration of the electronic device: read the configuration information item via the radiofrequency tag reader and determine a configuration of the electronic device as a function of the configuration information item read.

Abstract: The disclosure relates to a system embedded in an airplane comprising an electronic device intended to be inserted into a frame, a frame that can accommodate the electronic device, in which system the electronic device includes a radiofrequency tag reader, a radiofrequency tag, having a configuration information item, is fixed to the frame such that the radiofrequency tag reader can read the radiofrequency tag once the electronic device is inserted into the frame and the electronic device is adapted to, in a phase of configuration of the electronic device: read the configuration information item via the radiofrequency tag reader and determine a configuration of the electronic device as a function of the configuration information item read.

Abstract: 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.

Abstract: The invention relates to a monitoring system for an aircraft platform implementing a set of avionics functions using a plurality of heterogeneous hardware and software components, including: an acquisition module for operating parameters of the components, configured to implement a plurality of communication protocols adapted to query each the component; a storage module including a database, configured to collect and store operating parameters acquired by the acquisition module in the database, and; an interface module with a plurality of clients, including a query unit configured to query the database of the storage module and supply one or several of the parameters stored in the database in response to a request made by a client; the acquisition, storage and interface modules being arranged in a three-tier architecture.

Abstract: The disclosure relates to reconfigurable avionics equipment, subscribed to an onboard network such as an AFDX® network. The equipment has an architecture in two portions, a functional portion which makes it possible to perform the function proper to the piece of equipment and an interfacing portion, which allows the functional portion to communicate over the network. The interfacing portion includes a configuration file separate from the one used to configure the functional portion and able to be downloaded, using the network, independently of the latter.

Abstract: The subject matter disclosed herein relates an on-board network with nodes linked by wired links, the on-board network being partitioned into adjacent sub-networks, mutually segregated by security elements. Each sub-network can be equipped with access points allowing mobile terminals to connect to the sub-network by wireless links. The access points of adjacent sub-networks use different communication standards or distinct sets of transmission resources in such a way that the segregation between adjacent sub-networks is preserved.

Abstract: An aircraft control system including transducers connected by interface units to an avionics network, such as an AFDX network. Each transducer is directly connected to an interface unit local to the transducer. Each interface unit is a configurable unit and has a signal processing module converting data to a format suitable for transmission over the network. Each interface unit may be configurable, via software commands, to operate in an application session mode, a data-loading mode, or a maintenance mode. Each interface unit may be directly associated with one of the software applications of the aircraft control system. The network may include a lower bandwidth part where data communication is conducted over sampling ports only. Interface units may be configured or installed using a plug and play method.

Abstract: The disclosure relates to reconfigurable avionics equipment, subscribed to an onboard network such as an AFDX network. The equipment has an architecture in two portions, a functional portion which makes it possible to perform the function proper to the piece of equipment and an interfacing portion, which allows the functional portion to communicate over the network. The interfacing portion includes a configuration file separate from the one used to configure the functional portion and able to be downloaded, using the network, independently of the latter.

Abstract: The subject matter disclosed herein relates an on-board network with nodes linked by wired links, the on-board network being partitioned into adjacent sub-networks, mutually segregated by security elements. Each sub-network can be equipped with access points allowing mobile terminals to connect to the sub-network by wireless links. The access points of adjacent sub-networks use different communication standards or distinct sets of transmission resources in such a way that the segregation between adjacent sub-networks is preserved.

Abstract: The invention relates to a monitoring system for an aircraft platform implementing a set of avionics functions using a plurality of heterogeneous hardware and software components, including: an acquisition module for operating parameters of the components, configured to implement a plurality of communication protocols adapted to query each the component; a storage module including a database, configured to collect and store operating parameters acquired by the acquisition module in the database, and; an interface module with a plurality of clients, including a query unit configured to query the database of the storage module and supply one or several of the parameters stored in the database in response to a request made by a client; the acquisition, storage and interface modules being arranged in a three-tier architecture.

Abstract: 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.