Abstract: An antenna with polarization switching comprising a plurality of waveguides fed with radiofrequency signals and perforated with apertures disposed so as to illuminate radiating elements placed on mobile support means in a plane that is distant from the said apertures, it being possible for the said support means to be configured according to at least two distinct configurations. The radiating elements illuminated according to one and the same configuration are adjacent, the support means being adapted for orienting the radiating elements illuminated in a first configuration according to a different direction from the radiating elements illuminated in a second configuration. The antenna applies notably to the switching of antennas onboard objects moving on the ground required to undertake high-speed communications with a satellite, in particular a geostationary satellite.

Abstract: A method is provided for selectively, dynamically and adaptively jamming the third-party radio communications that are external to a radio communication network to be protected, which optimizes the effectiveness of the jamming of P predefined areas or positions in a network of transmitters, and which uses closed-loop control to limit fratricidal effects on certain platforms having telecommunication transmitters/receivers to be preserved.

Abstract: A configured aircraft flight management aid system comprises: means of interpretation receiving data taken from external instructions from an external control center, data relating to aircraft equipment failures, cabin problems and problems related to the environment of the aircraft; means of determination receiving data from the means of interpretation and determining at least one reference constraint associated with at least one parameter representative of a flight path, a reference constraint associated with a reference parameter comprising a new constraint, different from the initial constraint when the item of data effectively necessitates following a new path, different from the initial path, and a reference constraint comprising the initial constraint when the means of determination do not have access to any data relating to an event effectively necessitating following a new path; warning means generating a warning to an operator when the path actually flown does not comply with said reference constrai

Abstract: A method for securing communications in a network comprising at least one emitter terminal A and one receiver terminal B, comprises in combination at least the following steps: defining a measurable quantity that can be measured at the emitter A and the receiver B; normalizing and quantifying said defined quantity; initializing an initialization vector with said normalized and quantified quantity; using said initialization vector with a cryptographic key to randomly generate a set of consecutive frequencies to use for securing said communications between the emitter A and the receiver B; and incrementing the initialization vector by a given value after each pseudo-random generation time interval Itpa in order to generate a set of consecutive frequency values.

Abstract: The electronic computer according to the invention comprises: a storage case comprising a housing including an air inlet and an air outlet for the circulation of a flow of cooling air through the housing, an electronic motherboard comprising a first surface and a second surface, the second surface being provided with connectors for receiving electronic daughterboards, and an air channeling system configured so as to channel the air hitting the first surface of the electronic motherboard to bring it to the side of the second surface of the electronic motherboard. According to one aspect of the invention, the air channeling system is configured to spray the electronic daughterboards, so as to cool said electronic daughterboards through convection of the air.

Abstract: A system and method for modifying the carrier frequency of first and second signals associated with first and second sequences, respectively, of consecutive time intervals, comprises: first means determining two carrier frequencies respectively associated with each of the two signals based on one time interval or at least two consecutive and continuous time intervals, said time interval(s) belonging to a sequence of consecutive time intervals of known duration; and second means determining a first time interval or at least two first consecutive time intervals belonging to the first sequence, based on a second time interval belonging to the second sequence, by establishing a temporal correspondence between each end of said time interval of said second sequence and an interval of said first sequence including this end. The first means determines said carrier frequencies based on one time interval or at least two consecutive time intervals, belonging to said first sequence.

Abstract: A method is provided for the validation of a network by a checking module, the network comprising a plurality of routers, each of the routers comprising a plurality of output ports, each of the output ports of the routers being associated with a bandwidth budget, a priority latency budget and a plurality of network budget grains. The method comprises, for each of the ports of each of the routers, steps of: calculation of a latency consumed on the output port of the router on the basis of the network budget grains and the bandwidth budget; checking of the compatibility of the latency consumed on the output port with the priority latency budget grains of the output port of the router; and, transmission by the checking module of a signal indicating the result of the check.

Abstract: The invention relates to an on-board optoelectronic system to assist the taxiing of an aircraft on the taxiways of an airport, that includes: a database (2) of maps of the airport, a device (1) for positioning the aircraft, and a device (3) for generating first graphical data representing a “moving map”. a graphical data display device (4), a database (5) describing the features of the cockpit, a device (7) for generating second graphical data as a function of the said features, representing a zone of visibility from the cockpit by means of a mask (30), and means of superimposition (8) of the second graphical data on the first graphical data, connected to the display device (4).

Abstract: A method, and an associated device, is provided for the determination, by a flight management system of an aircraft, of a lateral trajectory of said aircraft on the basis of a predefined flight plan allowing consecutive conflicts to be resolved in an improved manner. This allows an improved lateral trajectory to be designed in the case where multiple trajectory conflicts exist. The trajectory obtained is closer to the flight plan defined by the pilot. The propagation of trajectory conflicts to the following flight segments is thus avoided. In fact, instead of propagating the trajectory conflict from one resolution to another, the method allows the conflict to be resolved in a space delimited at most by the input of the first conflict and the output of the last conflict.

Abstract: Energy management on board an aircraft includes: a plurality of thermal and electrical energy sources, a plurality of loads which are capable of being supplied with power by the various energy sources, among which at least one load is capable of being supplied with power by an electrical energy source and by a thermal energy source, and real-time management means for energy transfers from the various energy sources to the various loads as a function of the present and future energy requirement of the various loads and the present and future availability of the various sources, with the management means providing a permanent and standardized correlation between thermal and electrical energies.

Abstract: A computer equipment comprises a trackball used to point to objects on a screen of the equipment. A method for driving the computer equipment is also provided. The trackball comprises a moving part and a body inside which the moving part can be displaced, the computer being configured to display at least one object and a pointer on the screen. The trackball comprises means making it possible to exert a tangential force on the moving part, means driven by the computer. The computer is configured to modulate the force according to the shape of the object displayed and the position of the pointer relative to the object.

Abstract: System for receiving satellite signals jammed by at least one source of interference and by a thermal noise comprising means for receiving the said satellite signals, means for filtering the said satellite signals, in order to remove the disruption from the said sources of interference. The system also comprises first means for determining a first covariance matrix of the satellite signals, adding means for adding respectively a first coefficient to at least one element of the diagonal of the said first covariance matrix in order to obtain a second covariance matrix, second means for determining, on the basis of the said second covariance matrix, second coefficients used by the said filtering means. The system also comprises means for detecting a first power of the said thermal noise, third means for dynamic determination of the value of the said first coefficients, on the basis of the first power.

Abstract: A communications method for retransmission of at least one fragment of a lost or erroneous message from a terminal to a gateway over a communications network comprising a plurality of terminals, communicating over a demand assignment multiple access and comprising a control centre allocating the communications resource to the terminals, comprises: detection, by the gateway, of fragments of lost or erroneous messages and, when at least one fragment is detected, notification via the gateway to the control centre of the loss of at least one fragment; calculation, by the control centre, of a second allocation plan taking into account a new transmission of the fragment; notification by the gateway to the terminal of the loss of the fragment and notification by the control centre to the terminal of the second allocation plan; transmission by the terminal of the lost fragment according to the second allocation plan to the gateway.

Abstract: A satellite transmission system comprises at least: one satellite and two stations comprising transmission means transmitting simultaneously and in the same frequency band a first, high-bit-rate signal and a second, low-bit-rate signal, the second signal allowing changing of frequency of the carrier signal. The station(s) include reception means for receiving simultaneously and in the same frequency band the first and second signal. The system includes means for detecting interference on the frequency band. The transmission means and reception means respectively switch the transmission and reception of the second signal from a low bit rate to a medium bit rate and deactivate the transmission of the first signal in presence of interference, and the transmission means and reception means respectively switch the transmission and reception of the second signal from a medium bit rate to a low bit rate and activate transmission of the first signal in absence of interference.

Abstract: The invention relates to a system for assisting the pilot of an aircraft, which comprises aboard the aircraft: a computer, a set of sensors able to provide data to the computer and, a seat for the pilot equipped with haptic actuators controlled by the computer. The computer comprises means for controlling each actuator or groups of actuators independently of one another, as a function of the data provided by the sensors. The seat comprising a back and a cushion, the actuators of the back and of the cushion comprise single-axis mini-rams distributed in the back and the cushion of the seat, whose displacement axes are respectively perpendicular to the back and to the cushion of the seat.

Abstract: A method is provided for retransmitting fragmented packets for which a transference of retransmission credit is performed from one fragment onto the next. The method makes it possible to do away with the drawbacks of the methods existing by appreciably improving performance in terms of untransmitted packet rate and by making it possible to configure the distribution of the error probabilities for the fragments of an IP packet.

Abstract: A probe for measuring the total pressure of a flow and a method for implementing the probe is provided. The probe is intended to be fitted in an aircraft. The probe comprises a Pitot tube and means for reheating the probe assembly. The probe also comprises means for measuring a local temperature of regions of the Pitot tube likely to accumulate particles conveyed by the flow independently of the means for determining the average temperature of the probe. If the temperature delivered by the means for measuring a local temperature of regions of the Pitot tube likely to accumulate particles conveyed by the flow is less than the first reference temperature, then an additional reheating of regions of the Pitot tube likely to accumulate particles conveyed by the flow is triggered.

Abstract: A data input device is provided, implementing a potentiometer having a first and a second fixed connection point which are respectively situated at each of the ends of the potentiometer, a third fixed connection point situated at an intermediate position on the potentiometer and a fourth, mobile connection point forming a slider. The data input device comprises means converting a position of the slider into an electrical voltage, means for supplying a first fixed voltage to the potentiometer via the third connection point, means for supplying a current source to the potentiometer via the slider, means for measuring a voltage difference between the first and second connection points, the voltage difference forming the electrical voltage that represents the position of the slider.

Abstract: A method is provided for controlling a set of at least two satellites, designed to provide a service on a geostationary orbit, rendering said service on a non-geostationary orbit, in which means involved in the performance of said service, installed on board a satellite, are deactivated when the sun can damage it, and means involved in the performance of said service installed on board another satellite of the set are activated, when this is necessary to the continuity of the service.

Abstract: A probe for measuring a local angle of attack designed to be fixed to a wall and a method implementing the probe are provided. The probe comprises at least three pressure sampling ports disposed over a nose of the probe body, pressure measurement means associated with the pressure sampling ports and calculation means capable of determining an angle of attack of the flow with respect to the main direction of the probe body as a function of the pressures measured by the pressure measurement means. The calculation means are configured for choosing from amongst the pressure sampling ports those allowing the best measurement precision of the local angle of attack to be obtained and for calculating the local angle of attack with respect to the main direction using the pressure measurements carried out in the chosen pressure sampling ports.